diff --git a/src/common/tiglcommonfunctions.cpp b/src/common/tiglcommonfunctions.cpp
index 48feaa706..351467787 100644
--- a/src/common/tiglcommonfunctions.cpp
+++ b/src/common/tiglcommonfunctions.cpp
@@ -42,6 +42,9 @@
 #include "CTiglRelativelyPositionedComponent.h"
 #include "CTiglProjectPointOnCurveAtAngle.h"
 #include "CTiglBSplineAlgorithms.h"
+#include "CTiglPointsToBSplineInterpolation.h"
+#include "CFunctionToBspline.h"
+#include "tiglmathfunctions.h"
 
 #include "Standard_Version.hxx"
 
@@ -119,6 +122,7 @@
 #include <ShapeAnalysis_FreeBounds.hxx>
 
 
+
 #include <list>
 #include <algorithm>
 #include <cassert>
@@ -127,6 +131,7 @@
 
 #include "Debugging.h"
 
+
 namespace
 {
     struct IsSame
@@ -1173,6 +1178,155 @@ TopoDS_Wire BuildWireFromEdges(const TopoDS_Shape& edges)
     return result;
 }
 
+namespace
+{
+    class Circle : public tigl::MathFunc3d
+    {
+    public:
+        Circle(double radius): tigl::MathFunc3d(), m_radius(radius) {}
+
+        double valueX(double t) override
+        {
+            return 0.;
+        }
+
+        double valueY(double t) override
+        {
+            return m_radius*std::cos(t);
+        }
+
+        double valueZ(double t) override
+        {
+            return m_radius*std::sin(t);
+        }
+
+    private:
+          double m_radius;
+    };
+} //anonymos namespace
+
+opencascade::handle<Geom_BSplineCurve> ApproximateArcOfCircleToRationalBSpline(double radius, double uMin, double uMax,
+                                                                               double tol, double y_position, double z_position)
+{
+    if(radius==0){
+        throw tigl::CTiglError("Invalid geometry. Radius must be != 0.");
+    }
+    if(Abs(uMax-uMin)< tol){
+        throw tigl::CTiglError("Invalid geometry: Curve length must not be Zero.");
+    }
+    if(Abs(uMax-uMin)>(2.*M_PI))
+    {
+        throw tigl::CTiglError("Invalid geometry: Curve cannot be traversed more than once.");
+    }
+
+    Circle circle(radius);
+    int degree = 3;
+
+    auto curve = tigl::CFunctionToBspline(circle, uMin, uMax, degree, tol).Curve();
+    curve->Translate(gp_Vec(0.,y_position,z_position));
+
+    return curve;
+}
+
+TopoDS_Wire BuildWireRectangle(const double heightToWidthRatio, const double cornerRadius, const double tol)
+{
+    if(cornerRadius<0.||cornerRadius>0.5){
+        throw tigl::CTiglError("Invalid input for corner radius. Must be in range: 0 <= cornerRadius <= 0.5");
+    }
+
+    std::vector<Handle(Geom_BSplineCurve)> curves;
+
+    // build half upper line from gp_points
+    std::vector<gp_Pnt> linePntsUpperRightHalf;
+    linePntsUpperRightHalf.push_back(gp_Pnt(0.,0.,0.5*heightToWidthRatio));
+    linePntsUpperRightHalf.push_back(gp_Pnt(0.,0.5-cornerRadius,0.5*heightToWidthRatio));
+    opencascade::handle<Geom_BSplineCurve> lowerLineRightHalf =
+            tigl::CTiglPointsToBSplineInterpolation(linePntsUpperRightHalf).Curve();
+    curves.push_back(lowerLineRightHalf);
+
+    if (!(cornerRadius == 0.0)){
+        //build upper right arc
+        double y0 = 0.5 - cornerRadius;
+        double z0 = 0.5 * heightToWidthRatio - cornerRadius;
+        auto arcCurve = ApproximateArcOfCircleToRationalBSpline(cornerRadius, 0., M_PI/2., tol, y0, z0);
+        arcCurve->Reverse();
+        curves.push_back(arcCurve);
+    }
+
+    // build right line from gp_Pnts
+    std::vector<gp_Pnt> linePnts_right;
+    linePnts_right.push_back(gp_Pnt(0., 0.5, 0.5 * heightToWidthRatio - cornerRadius));
+    linePnts_right.push_back(gp_Pnt(0., 0.5, -0.5 * heightToWidthRatio + cornerRadius));
+    opencascade::handle<Geom_BSplineCurve> rightLine = tigl::CTiglPointsToBSplineInterpolation(linePnts_right).Curve();
+    curves.push_back(rightLine);
+
+    if (!(cornerRadius == 0.0)){
+        //build lower right arc
+        double y0 = 0.5 - cornerRadius;
+        double z0 = - 0.5 * heightToWidthRatio + cornerRadius;
+        auto arcCurve = ApproximateArcOfCircleToRationalBSpline(cornerRadius, M_PI*(3./2.), M_PI*2., tol, y0, z0);
+        arcCurve->Reverse();
+        curves.push_back(arcCurve);
+    }
+
+    // build lower line from gp_points
+    std::vector<gp_Pnt> linePnts_lower;
+    linePnts_lower.push_back(gp_Pnt(0.,(0.5-cornerRadius),-0.5*heightToWidthRatio));
+    linePnts_lower.push_back(gp_Pnt(0.,(-0.5+cornerRadius),-0.5*heightToWidthRatio));
+    opencascade::handle<Geom_BSplineCurve> lowerLine = tigl::CTiglPointsToBSplineInterpolation(linePnts_lower).Curve();
+
+    curves.push_back(lowerLine);
+
+    if (!(cornerRadius == 0.)){
+        // build lower left arc
+        double y0 = - 0.5 + cornerRadius;
+        double z0 = -0.5 * heightToWidthRatio + cornerRadius;
+        auto arcCurve = ApproximateArcOfCircleToRationalBSpline(cornerRadius, M_PI, M_PI*(3./2.), tol, y0, z0);
+        arcCurve->Reverse();
+        curves.push_back(arcCurve);
+    }
+
+    //build left line from gp_points
+    std::vector<gp_Pnt> linePnts_left;
+    linePnts_left.push_back(gp_Pnt(0.,-0.5,-0.5 * heightToWidthRatio + cornerRadius));
+    linePnts_left.push_back(gp_Pnt(0.,-0.5,0.5 * heightToWidthRatio - cornerRadius));
+    opencascade::handle<Geom_BSplineCurve> leftLine = tigl::CTiglPointsToBSplineInterpolation(linePnts_left).Curve();
+    curves.push_back(leftLine);
+
+    if (!(cornerRadius == 0.)) {
+        // build upper left arc
+        double y0 = - 0.5 + cornerRadius;
+        double z0 = 0.5 * heightToWidthRatio - cornerRadius;
+        auto arcCurve = ApproximateArcOfCircleToRationalBSpline(cornerRadius, M_PI/2., M_PI, tol, y0, z0);
+        arcCurve->Reverse();
+        curves.push_back(arcCurve);
+    }
+
+    // build half upper line from gp_points
+    std::vector<gp_Pnt> linePntsUpperLeftHalf;
+    linePntsUpperLeftHalf.push_back(gp_Pnt(0.,-(0.5-cornerRadius),0.5*heightToWidthRatio));
+    linePntsUpperLeftHalf.push_back(gp_Pnt(0.,0.,0.5*heightToWidthRatio));
+    opencascade::handle<Geom_BSplineCurve> upperLineLeftHalf =
+            tigl::CTiglPointsToBSplineInterpolation(linePntsUpperLeftHalf).Curve();
+    curves.push_back(upperLineLeftHalf);
+
+    opencascade::handle<Geom_BSplineCurve> curve = tigl::CTiglBSplineAlgorithms::concatCurves(curves);
+
+    // workaround for lofting algorithm not working with  curves of degree '1' (i.e. concatenated lines)
+    // if guide curves are involved, the lofter doesn't generate a valid geometry without thowing an error
+    // This only occurs if the cornerRadius is zero and the profile is a rectangle, which in theory could
+    // just have degree 1.
+    if ((curve->Degree())<2){
+        curve->IncreaseDegree(2);
+    }
+
+    TopoDS_Wire wire;
+    if (!curve.IsNull()) {
+        wire = BuildWireFromEdges(BRepBuilderAPI_MakeEdge(curve).Edge());
+    }
+    return wire;
+}
+
 void BuildWiresFromConnectedEdges(const TopoDS_Shape& shape, TopTools_ListOfShape& wireList)
 {
     // get list of edges from passed shape
diff --git a/src/common/tiglcommonfunctions.h b/src/common/tiglcommonfunctions.h
index 5dd8e42e7..487597107 100644
--- a/src/common/tiglcommonfunctions.h
+++ b/src/common/tiglcommonfunctions.h
@@ -46,6 +46,8 @@
 #include <algorithm>
 #include "UniquePtr.h"
 
+
+
 typedef std::map<std::string, PNamedShape> ShapeMap;
 
 // helper function for std::find
@@ -270,6 +272,34 @@ TIGL_EXPORT TopoDS_Wire BuildWire(const gp_Pnt& p1, const gp_Pnt& p2);
 // Method for building a wire out of the edges from the passed geometry
 TIGL_EXPORT TopoDS_Wire BuildWireFromEdges(const TopoDS_Shape& edges);
 
+/**
+ * @brief ApproximateArcOfCircleToRationalBSpline The result of this function is a non-rational
+ * B-Spline curve that approximates an arc of circle in the y-z plane.
+ * Its center is given by the y- and z-position.
+ * The angle is given in rad.
+ * The direction of rotation is counter-clockwise, starting with alpha=0 on the positive y-axis,  with z=0.
+ * @param cornerRadius      Radius of the circle
+ * @param uMin              Starting parameter in rad. Range: [0,2*Pi]
+ * @param uMax
+ * @param tol               Tolerance
+ * @param y_position
+ * @param z_position
+ * @return opencascade::handle<Geom_BSplineCurve>
+ */
+TIGL_EXPORT opencascade::handle<Geom_BSplineCurve> ApproximateArcOfCircleToRationalBSpline(double cornerRadius, double uMin = 0, double uMax = M_PI/4 ,
+                                                                                           double tol = 1e-6, double y_position = 0., double z_position = 0.);
+
+/**
+ * @brief BuildWireRectangle Builds a rectangular wire in (y,z) - plane with width 1, center of coordinate
+ * system is the center of the rectangle
+ * @param heightToWidthRatio
+ * @param cornerRadius
+ * @param tol
+ * @return TopoDS_Wire
+ */
+TIGL_EXPORT TopoDS_Wire BuildWireRectangle(const double heightToWidthRatio, const double cornerRadius=0.0,
+                                           const double tol=Precision::Approximation());
+
 // Returns a list of wires built from all connected edges in the passed shape
 TIGL_EXPORT void BuildWiresFromConnectedEdges(const TopoDS_Shape& shape, TopTools_ListOfShape& wireList);
 
@@ -359,7 +389,7 @@ TIGL_EXPORT double NormalizeAngleDeg(double angleDeg);
 // Creates a linear spaces array but with some additional breaking points
 // If the breaking points are very close to a point, the point will be replaced
 // Else, the breaking point will be inserted
-TIGL_EXPORT std::vector<double> LinspaceWithBreaks(double umin, double umax, size_t n_values, const std::vector<double>& breaks);
+TIGL_EXPORT std::vector<double> LinspaceWithBreaks(double umin, double umax, size_t n_values, const std::vector<double>& breaks = {});
 
 // Transforms a shape accourding to the given coordinate transformation
 TIGL_EXPORT TopoDS_Shape TransformedShape(const tigl::CTiglTransformation& transformationToGlobal, TiglCoordinateSystem cs, const TopoDS_Shape& shape);
diff --git a/src/fuselage/CCPACSFuselageProfile.cpp b/src/fuselage/CCPACSFuselageProfile.cpp
index e92153d0e..c099a1466 100644
--- a/src/fuselage/CCPACSFuselageProfile.cpp
+++ b/src/fuselage/CCPACSFuselageProfile.cpp
@@ -175,71 +175,101 @@ TopoDS_Wire CCPACSFuselageProfile::GetWire(bool forceClosed) const
 // fuselage profile element transformation.
 void CCPACSFuselageProfile::BuildWires(WireCache& cache) const
 {
-    if (!m_pointList_choice1)
-        throw CTiglError("Currently only fuselage profiles defined by pointList are supported.");
-    if (GetNumPoints() < 2) {
-        throw CTiglError("Number of points is less than 2 in CCPACSFuselageProfile::BuildWire", TIGL_ERROR);
+    if(m_pointList_choice1){
+        BuildWiresPointList(cache);
+        return;
     }
-
-    auto points = m_pointList_choice1->AsVector();
-    auto params = m_pointList_choice1->GetParamsAsMap();
-    auto kinks  = m_pointList_choice1->GetKinksAsVector();
-    if (mirrorSymmetry) {
-        SymmetrizeFuselageProfile(points, params, kinks);
+    if(m_standardProfile_choice3){
+        if(m_standardProfile_choice3->GetRectangle_choice1()){
+            BuildWiresRectangle(cache);
+            return;
+        }
     }
+    throw CTiglError("Currently only fuselage profiles defined by pointList and rectangular fuselage profiles are supported.");
+}
 
-    // Build the B-Spline
-    auto occPoints = OccArray(points);
+// Builds the fuselage profile wire from point list.
+void CCPACSFuselageProfile::BuildWiresPointList(WireCache& cache) const
+{
+        if (GetNumPoints() < 2) {
+            throw CTiglError("Number of points is less than 2 in CCPACSFuselageProfile::BuildWire", TIGL_ERROR);
+        }
 
-    // we always want to include the endpoint, if it's the same as the startpoint
-    // we use the middle to enforce closing of the spline
-    gp_Pnt pStart = points.front().Get_gp_Pnt();
-    gp_Pnt pEnd   = points.back().Get_gp_Pnt();
+        auto points = m_pointList_choice1->AsVector();
+        auto params = m_pointList_choice1->GetParamsAsMap();
+        auto kinks  = m_pointList_choice1->GetKinksAsVector();
+        if (mirrorSymmetry) {
+            SymmetrizeFuselageProfile(points, params, kinks);
+        }
 
-    // this check allows some tolerance, based on the absolute size of the profile
-    if (pStart.Distance(pEnd) < 0.005 * CTiglBSplineAlgorithms::scale(occPoints->Array1())) {
-        gp_Pnt pMiddle = 0.5 * (pStart.XYZ() + pEnd.XYZ());
-        occPoints->SetValue(occPoints->Lower(), pMiddle);
-        occPoints->SetValue(occPoints->Upper(), pMiddle);
-    }
+        // Build the B-Spline
+        auto occPoints = OccArray(points);
 
-    // Here, the B-spline is reparameterized based on the CPACS profile after setting it up at first for accuracy reasons
-    // Also, a tolerance is passed used for knot insertion and removal during the reparameterization algorithm
-    CTiglInterpolatePointsWithKinks interp(occPoints, kinks, params, 0.5, 3, CTiglInterpolatePointsWithKinks::Algo::InterpolateFirstThenReparametrize, 1e-8);
-    auto spline = interp.Curve();
+        // we always want to include the endpoint, if it's the same as the startpoint
+        // we use the middle to enforce closing of the spline
+        gp_Pnt pStart = points.front().Get_gp_Pnt();
+        gp_Pnt pEnd   = points.back().Get_gp_Pnt();
 
-    if (mirrorSymmetry) {
-        double umin = spline->FirstParameter();
-        double umax = spline->LastParameter();
-        spline      = CTiglBSplineAlgorithms::trimCurve(spline, umin, 0.5 * (umin + umax));
-        CTiglBSplineAlgorithms::reparametrizeBSpline(*spline, umin, umax);
-    }
+        // this check allows some tolerance, based on the absolute size of the profile
+        if (pStart.Distance(pEnd) < 0.005 * CTiglBSplineAlgorithms::scale(occPoints->Array1())) {
+            gp_Pnt pMiddle = 0.5 * (pStart.XYZ() + pEnd.XYZ());
+            occPoints->SetValue(occPoints->Lower(), pMiddle);
+            occPoints->SetValue(occPoints->Upper(), pMiddle);
+        }
 
-    // Reparamaterization based on a ParamMap defined in the CPACS file within CTiglInterpolatePointsWithKinks does not get along with reparametrizeBSplineNiceKnots.
-    // The geometry is changed in a way that is not acceptable anymore. However out of performance reasons, the feature should not be rejected in the most cases.
-    // Due to those conflicts, the function is only called, when there are no parameters defined in the CPACS file:
-    if (params.empty()) {
-        // we reparametrize the spline to get better performing lofts.
-        // there might be a small accuracy loss though.
-        spline = CTiglBSplineAlgorithms::reparametrizeBSplineNiceKnots(spline).curve;
-     }
-
-    // Create wires
-    TopoDS_Edge edge = BRepBuilderAPI_MakeEdge(spline).Edge();
-    BRepBuilderAPI_MakeWire builder1(edge);
-    TopoDS_Wire tempWireOriginal = builder1.Wire();
-
-    BRepBuilderAPI_MakeWire builder2(edge);
-    if (!spline->IsClosed()) {
-        builder2.Add(BRepBuilderAPI_MakeEdge(spline->EndPoint(), spline->StartPoint()));
-    }
-    TopoDS_Wire tempWireClosed = builder2.Wire();
-    if (tempWireClosed.IsNull() == Standard_True || tempWireOriginal.IsNull() == Standard_True) {
-        throw CTiglError("TopoDS_Wire is null in CCPACSFuselageProfile::BuildWire", TIGL_ERROR);
-    }
+        // Here, the B-spline is reparameterized based on the CPACS profile after setting it up at first for accuracy reasons
+        // Also, a tolerance is passed used for knot insertion and removal during the reparameterization algorithm
+        CTiglInterpolatePointsWithKinks interp(occPoints, kinks, params, 0.5, 3, CTiglInterpolatePointsWithKinks::Algo::InterpolateFirstThenReparametrize, 1e-8);
+        auto spline = interp.Curve();
 
-    cache.closed   = tempWireClosed;
-    cache.original = tempWireOriginal;
+        if (mirrorSymmetry) {
+            double umin = spline->FirstParameter();
+            double umax = spline->LastParameter();
+            spline      = CTiglBSplineAlgorithms::trimCurve(spline, umin, 0.5 * (umin + umax));
+            CTiglBSplineAlgorithms::reparametrizeBSpline(*spline, umin, umax);
+        }
+
+        // Reparamaterization based on a ParamMap defined in the CPACS file within CTiglInterpolatePointsWithKinks does not get along with reparametrizeBSplineNiceKnots.
+        // The geometry is changed in a way that is not acceptable anymore. However out of performance reasons, the feature should not be rejected in the most cases.
+        // Due to those conflicts, the function is only called, when there are no parameters defined in the CPACS file:
+        if (params.empty()) {
+            // we reparametrize the spline to get better performing lofts.
+            // there might be a small accuracy loss though.
+            spline = CTiglBSplineAlgorithms::reparametrizeBSplineNiceKnots(spline).curve;
+         }
+
+        // Create wires
+        TopoDS_Edge edge = BRepBuilderAPI_MakeEdge(spline).Edge();
+        BRepBuilderAPI_MakeWire builder1(edge);
+        TopoDS_Wire tempWireOriginal = builder1.Wire();
+
+        BRepBuilderAPI_MakeWire builder2(edge);
+        if (!spline->IsClosed()) {
+            builder2.Add(BRepBuilderAPI_MakeEdge(spline->EndPoint(), spline->StartPoint()));
+        }
+        TopoDS_Wire tempWireClosed = builder2.Wire();
+        if (tempWireClosed.IsNull() == Standard_True || tempWireOriginal.IsNull() == Standard_True) {
+            throw CTiglError("TopoDS_Wire is null in CCPACSFuselageProfile::BuildWire", TIGL_ERROR);
+        }
+
+        cache.closed   = tempWireClosed;
+        cache.original = tempWireOriginal;
+}
+
+//Builds the fuselage profile wire from heightToWidthRatio and cornerRadius with a tolerance of 1e-3 for the wire
+void CCPACSFuselageProfile::BuildWiresRectangle(WireCache& cache) const
+{
+    if(!m_standardProfile_choice3->GetRectangle_choice1()){
+        throw CTiglError("CCPACSFuselageProfile::BuildWire", TIGL_ERROR);
+    }
+    //Get Paramenters
+    auto& rectangle_profile = *m_standardProfile_choice3->GetRectangle_choice1();
+    double heightToWidthRatio = rectangle_profile.GetHeightToWidthRatio().GetValue();
+    double radius = (rectangle_profile.GetCornerRadius())? *rectangle_profile.GetCornerRadius() : 0. ;
+    //Build wire
+    TopoDS_Wire wire = BuildWireRectangle(heightToWidthRatio,radius, 1e-3);
+    cache.closed = wire;
+    cache.original = wire;
 }
 
 // Transforms a point by the fuselage profile transformation
@@ -276,31 +306,44 @@ gp_Pnt CCPACSFuselageProfile::GetPoint(double zeta) const
 
 void CCPACSFuselageProfile::BuildDiameterPoints(DiameterPointsCache& cache) const
 {
-    if (!m_pointList_choice1)
-        throw CTiglError("No pointlist specified");
-    const std::vector<CTiglPoint>& coordinates = m_pointList_choice1->AsVector();
-
-    if (mirrorSymmetry) {
-        cache.start = coordinates[0].Get_gp_Pnt();
-        cache.end   = coordinates[coordinates.size() - 1].Get_gp_Pnt();
-    }
-    else {
-        // compute starting diameter point
-        gp_Pnt firstPnt = coordinates[0].Get_gp_Pnt();
-        gp_Pnt lastPnt  = coordinates[coordinates.size() - 1].Get_gp_Pnt();
-        double x        = (firstPnt.X() + lastPnt.X()) / 2.;
-        double y        = (firstPnt.Y() + lastPnt.Y()) / 2.;
-        double z        = (firstPnt.Z() + lastPnt.Z()) / 2.;
-        cache.start     = gp_Pnt(x, y, z);
-
-        // find the point with the max dist to starting point
-        cache.end = cache.start;
-        for (std::vector<CTiglPoint>::const_iterator it = coordinates.begin(); it != coordinates.end(); ++it) {
-            gp_Pnt point = it->Get_gp_Pnt();
-            if (cache.start.Distance(point) > cache.start.Distance(cache.end)) {
-                cache.end = point;
+    if (m_pointList_choice1){
+        const std::vector<CTiglPoint>& coordinates = m_pointList_choice1->AsVector();
+        if (mirrorSymmetry) {
+            cache.start = coordinates[0].Get_gp_Pnt();
+            cache.end   = coordinates[coordinates.size() - 1].Get_gp_Pnt();
+        }
+        else {
+            // compute starting diameter point
+            gp_Pnt firstPnt = coordinates[0].Get_gp_Pnt();
+            gp_Pnt lastPnt  = coordinates[coordinates.size() - 1].Get_gp_Pnt();
+            double x        = (firstPnt.X() + lastPnt.X()) / 2.;
+            double y        = (firstPnt.Y() + lastPnt.Y()) / 2.;
+            double z        = (firstPnt.Z() + lastPnt.Z()) / 2.;
+            cache.start     = gp_Pnt(x, y, z);
+
+            // find the point with the max dist to starting point
+            cache.end = cache.start;
+            for (std::vector<CTiglPoint>::const_iterator it = coordinates.begin(); it != coordinates.end(); ++it) {
+                gp_Pnt point = it->Get_gp_Pnt();
+                if (cache.start.Distance(point) > cache.start.Distance(cache.end)) {
+                    cache.end = point;
+                }
             }
         }
+    } else if (m_standardProfile_choice3)
+    {
+        if(m_standardProfile_choice3->GetRectangle_choice1())
+        {
+           //Get Paramenters
+           auto& rectangle_profile = *m_standardProfile_choice3->GetRectangle_choice1();
+           double heightToWidthRatio = rectangle_profile.GetHeightToWidthRatio().GetValue();
+           cache.start = gp_Pnt(0., 0, 0.5 * heightToWidthRatio);
+           cache.end = gp_Pnt(0., 0, -0.5 * heightToWidthRatio);
+        } else {
+            throw CTiglError("Unknown or unsupported profile type");
+        }
+    } else {
+        throw CTiglError("Unknown or unsupported profile type");
     }
 }
 
diff --git a/src/fuselage/CCPACSFuselageProfile.h b/src/fuselage/CCPACSFuselageProfile.h
index 22dea1e97..d38895557 100644
--- a/src/fuselage/CCPACSFuselageProfile.h
+++ b/src/fuselage/CCPACSFuselageProfile.h
@@ -90,6 +90,12 @@ class CCPACSFuselageProfile : public generated::CPACSProfileGeometry
     // fuselage profile transformation.
     void BuildWires(WireCache& cache) const;
 
+    //Builds the fuselage profile wires from point list
+    void BuildWiresPointList(WireCache& cache) const;
+
+    //Builds the fuselage profile wires from height to width ratio and corner radius
+    void BuildWiresRectangle(WireCache& cache) const;
+
     // Helper function to determine the "diameter" (the wing profile chord line equivalent)
     // which is defined as the line intersecting Point1 and Point2
     //
diff --git a/src/geometry/CTiglPointsToBSplineInterpolation.cpp b/src/geometry/CTiglPointsToBSplineInterpolation.cpp
index 37adbcf40..1709cca94 100644
--- a/src/geometry/CTiglPointsToBSplineInterpolation.cpp
+++ b/src/geometry/CTiglPointsToBSplineInterpolation.cpp
@@ -20,6 +20,7 @@
 
 #include "CTiglError.h"
 #include "CTiglBSplineAlgorithms.h"
+#include "tiglcommonfunctions.h"
 
 #include <BSplCLib.hxx>
 #include <math_Gauss.hxx>
@@ -76,6 +77,11 @@ CTiglPointsToBSplineInterpolation::CTiglPointsToBSplineInterpolation(const Handl
     }
 }
 
+CTiglPointsToBSplineInterpolation::CTiglPointsToBSplineInterpolation(const std::vector<gp_Pnt>& points,
+                                                                     unsigned int maxDegree, bool continuousIfClosed)
+    : CTiglPointsToBSplineInterpolation(OccArray(points), maxDegree, continuousIfClosed)
+{}
+
 CTiglPointsToBSplineInterpolation::CTiglPointsToBSplineInterpolation(const Handle(TColgp_HArray1OfPnt) & points,
                                                                      const std::vector<double>& parameters,
                                                                      unsigned int maxDegree, bool continuousIfClosed)
@@ -101,6 +107,12 @@ CTiglPointsToBSplineInterpolation::CTiglPointsToBSplineInterpolation(const Handl
     }
 }
 
+CTiglPointsToBSplineInterpolation::CTiglPointsToBSplineInterpolation(const std::vector<gp_Pnt>& points,
+                                                                     const std::vector<double>& parameters,
+                                                                     unsigned int maxDegree, bool continuousIfClosed)
+    : CTiglPointsToBSplineInterpolation(OccArray(points), parameters, maxDegree, continuousIfClosed)
+{}
+
 Handle(Geom_BSplineCurve) CTiglPointsToBSplineInterpolation::Curve() const
 {
     int degree = static_cast<int>(Degree());
diff --git a/src/geometry/CTiglPointsToBSplineInterpolation.h b/src/geometry/CTiglPointsToBSplineInterpolation.h
index ec6f0332d..874e81caa 100644
--- a/src/geometry/CTiglPointsToBSplineInterpolation.h
+++ b/src/geometry/CTiglPointsToBSplineInterpolation.h
@@ -39,10 +39,16 @@ class CTiglPointsToBSplineInterpolation
     TIGL_EXPORT CTiglPointsToBSplineInterpolation(const Handle(TColgp_HArray1OfPnt) & points,
                                                   unsigned int maxDegree = 3, bool continuousIfClosed = false);
 
+    TIGL_EXPORT CTiglPointsToBSplineInterpolation(const std::vector<gp_Pnt>& points, unsigned int maxDegree = 3,
+                                                  bool continuousIfClosed = false);
+
     TIGL_EXPORT CTiglPointsToBSplineInterpolation(const Handle(TColgp_HArray1OfPnt) & points,
                                                   const std::vector<double>& parameters, unsigned int maxDegree = 3,
                                                   bool continuousIfClosed = false);
 
+    TIGL_EXPORT CTiglPointsToBSplineInterpolation(const std::vector<gp_Pnt>& points, const std::vector<double>& parameters, unsigned int maxDegree = 3,
+                                                  bool continuousIfClosed = false);
+
     /// Returns the interpolation curve
     TIGL_EXPORT Handle(Geom_BSplineCurve) Curve() const;
 
diff --git a/tests/unittests/TestData/simpletest_standard_profile_rectangle_circle_guides.cpacs.xml b/tests/unittests/TestData/simpletest_standard_profile_rectangle_circle_guides.cpacs.xml
new file mode 100644
index 000000000..7820d8fc9
--- /dev/null
+++ b/tests/unittests/TestData/simpletest_standard_profile_rectangle_circle_guides.cpacs.xml
@@ -0,0 +1,619 @@
+<?xml version="1.0" encoding="utf-8"?>
+<cpacs xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="http://cpacs.googlecode.com/files/CPACS_21_Schema.xsd">
+  <header>
+    <name>Cpacs2Test</name>
+    <description>Simple Wing for unit testing</description>
+    <creator>Martin Siggel</creator>
+    <timestamp>2012-10-09T15:12:47</timestamp>
+    <version>0.5.0</version>
+    <cpacsVersion>3.2</cpacsVersion>
+    <updates>
+      <update>
+        <modification>Converted to cpacs 3.0 using cpacs2to3 - does not include structure update</modification>
+        <creator>cpacs2to3</creator>
+        <timestamp>2018-01-15T09:22:57</timestamp>
+        <version>0.2</version>
+        <cpacsVersion>3.0</cpacsVersion>
+      </update>
+      <update>
+        <modification>Added missing UIDs.</modification>
+        <creator>fix_errors.py</creator>
+        <timestamp>2019-04-29T20:48:26</timestamp>
+        <version>0.3.0</version>
+        <cpacsVersion>3.0</cpacsVersion>
+      </update>
+      <update>
+        <modification>Converted to CPACS 3.1 using cpacs2to3</modification>
+        <creator>cpacs2to3</creator>
+        <timestamp>2020-04-26T02:01:33</timestamp>
+        <version>0.4.0</version>
+        <cpacsVersion>3.1</cpacsVersion>
+      </update>
+      <update>
+        <modification>Converted to CPACS 3.2 using cpacs2to3</modification>
+        <creator>cpacs2to3</creator>
+        <timestamp>2021-04-23T18:02:00</timestamp>
+        <version>0.5.0</version>
+        <cpacsVersion>3.2</cpacsVersion>
+      </update>
+    </updates>
+  </header>
+  <vehicles>
+    <aircraft>
+      <model uID="Cpacs2Test">
+        <name>Cpacs2Test</name>
+        <reference>
+          <area>1</area>
+          <length>1</length>
+          <point uID="Cpacs2Test_point1">
+            <x>0</x>
+            <y>0</y>
+            <z>0</z>
+          </point>
+        </reference>
+        <fuselages>
+          <fuselage uID="SimpleFuselage">
+            <name>name</name>
+            <description>description</description>
+            <transformation uID="SimpleFuselage_transformation1">
+              <scaling uID="SimpleFuselage_transformation1_scaling1">
+                <x>1.0</x>
+                <y>0.5</y>
+                <z>0.5</z>
+              </scaling>
+              <rotation uID="SimpleFuselage_transformation1_rotation1">
+                <x>0.0</x>
+                <y>0.0</y>
+                <z>0.0</z>
+              </rotation>
+              <translation refType="absLocal" uID="SimpleFuselage_transformation1_translation1">
+                <x>0.0</x>
+                <y>0.0</y>
+                <z>0.0</z>
+              </translation>
+            </transformation>
+            <sections>
+              <section uID="D150_Fuselage_1Section1ID">
+                <name>D150_Fuselage_1Section1</name>
+                <transformation uID="D150_Fuselage_1Section1ID_transformation1">
+                  <scaling uID="D150_Fuselage_1Section1ID_transformation1_scaling1">
+                    <x>1.0</x>
+                    <y>1.0</y>
+                    <z>1.0</z>
+                  </scaling>
+                  <rotation uID="D150_Fuselage_1Section1ID_transformation1_rotation1">
+                    <x>0.0</x>
+                    <y>0.0</y>
+                    <z>0.0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="D150_Fuselage_1Section1ID_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="D150_Fuselage_1Section1IDElement1">
+                    <name>D150_Fuselage_1Section1</name>
+                    <profileUID>fuselageCircleProfileuID</profileUID>
+                    <transformation uID="D150_Fuselage_1Section1IDElement1_transformation1">
+                      <scaling uID="D150_Fuselage_1Section1IDElement1_transformation1_scaling1">
+                        <x>1.0</x>
+                        <y>1.0</y>
+                        <z>1.0</z>
+                      </scaling>
+                      <rotation uID="D150_Fuselage_1Section1IDElement1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="D150_Fuselage_1Section1IDElement1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="D150_Fuselage_1Section2ID">
+                <name>D150_Fuselage_1Section2</name>
+                <transformation uID="D150_Fuselage_1Section2ID_transformation1">
+                  <scaling uID="D150_Fuselage_1Section2ID_transformation1_scaling1">
+                    <x>1.0</x>
+                    <y>1.0</y>
+                    <z>1.0</z>
+                  </scaling>
+                  <rotation uID="D150_Fuselage_1Section2ID_transformation1_rotation1">
+                    <x>0.0</x>
+                    <y>0.0</y>
+                    <z>0.0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="D150_Fuselage_1Section2ID_transformation1_translation1">
+                    <x>0.5</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="D150_Fuselage_1Section2IDElement1">
+                    <name>D150_Fuselage_1Section2</name>
+                    <profileUID>fuselageRectangleProfileuID</profileUID>
+                    <transformation uID="D150_Fuselage_1Section2IDElement1_transformation1">
+                      <scaling uID="D150_Fuselage_1Section2IDElement1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="D150_Fuselage_1Section2IDElement1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="D150_Fuselage_1Section2IDElement1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="D150_Fuselage_1Section3ID">
+                <name>D150_Fuselage_1Section3</name>
+                <transformation uID="D150_Fuselage_1Section3ID_transformation1">
+                  <scaling uID="D150_Fuselage_1Section3ID_transformation1_scaling1">
+                    <x>1.0</x>
+                    <y>1.0</y>
+                    <z>1.0</z>
+                  </scaling>
+                  <rotation uID="D150_Fuselage_1Section3ID_transformation1_rotation1">
+                    <x>0.0</x>
+                    <y>0.0</y>
+                    <z>0.0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="D150_Fuselage_1Section3ID_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="D150_Fuselage_1Section3IDElement1">
+                    <name>D150_Fuselage_1Section3</name>
+                    <profileUID>fuselageRectangle1ProfileuID</profileUID>
+                    <transformation uID="D150_Fuselage_1Section3IDElement1_transformation1">
+                      <scaling uID="D150_Fuselage_1Section3IDElement1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="D150_Fuselage_1Section3IDElement1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="D150_Fuselage_1Section3IDElement1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+            </sections>
+            <positionings>
+              <positioning uID="D150_Fuselage_1Positioning1ID">
+                <name>D150_Fuselage_1Positioning1</name>
+                <length>-0.5</length>
+                <sweepAngle>90</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <toSectionUID>D150_Fuselage_1Section1ID</toSectionUID>
+              </positioning>
+              <positioning uID="D150_Fuselage_1Positioning3ID">
+                <name>D150_Fuselage_1Positioning3</name>
+                <length>2</length>
+                <sweepAngle>90</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <fromSectionUID>D150_Fuselage_1Section1ID</fromSectionUID>
+                <toSectionUID>D150_Fuselage_1Section3ID</toSectionUID>
+              </positioning>
+            </positionings>
+            <segments>
+              <segment uID="segmentD150_Fuselage_1Segment2ID">
+                <name>D150_Fuselage_1Segment2</name>
+                <fromElementUID>D150_Fuselage_1Section1IDElement1</fromElementUID>
+                <guideCurves>
+                    <guideCurve uID= "D150_Fuselage_1_Segment2_guide0">
+                      <name>D150_Fuselage_1_Segment2_guide0</name>
+                      <guideCurveProfileUID>guideCurveProfileFuselage</guideCurveProfileUID>
+                      <fromRelativeCircumference>0</fromRelativeCircumference>
+                      <toRelativeCircumference>0</toRelativeCircumference>
+                    </guideCurve>
+                    <guideCurve uID= "D150_Fuselage_1_Segment2_guide1">
+                      <name>D150_Fuselage_1_Segment2_guide1</name>
+                      <guideCurveProfileUID>guideCurveProfileFuselage</guideCurveProfileUID>
+                      <fromRelativeCircumference>0.333</fromRelativeCircumference>
+                      <toRelativeCircumference>0.333</toRelativeCircumference>
+                    </guideCurve>
+                    <guideCurve uID= "D150_Fuselage_1_Segment2_guide2">
+                      <name>D150_Fuselage_1_Segment2_guide2</name>
+                      <guideCurveProfileUID>guideCurveProfileFuselage</guideCurveProfileUID>
+                      <fromRelativeCircumference>0.666</fromRelativeCircumference>
+                      <toRelativeCircumference>0.666</toRelativeCircumference>
+                    </guideCurve>
+                    <guideCurve uID= "D150_Fuselage_1_Segment2_guide3">
+                      <name>D150_Fuselage_1_Segment2_guide3</name>
+                      <guideCurveProfileUID>guideCurveProfileFuselage</guideCurveProfileUID>
+                      <fromRelativeCircumference>1</fromRelativeCircumference>
+                      <toRelativeCircumference>1</toRelativeCircumference>
+                    </guideCurve>
+                </guideCurves>
+                <toElementUID>D150_Fuselage_1Section2IDElement1</toElementUID>
+              </segment>
+              <segment uID="segmentD150_Fuselage_1Segment3ID">
+                <name>D150_Fuselage_1Segment3</name>
+                <fromElementUID>D150_Fuselage_1Section2IDElement1</fromElementUID>
+                <guideCurves>
+                    <guideCurve uID="D150_Fuselage_1_Segment3_guide0">
+                      <name>D150_Fuselage_1_Segment3_guide0</name>
+                      <guideCurveProfileUID>guideCurveProfileFuselage</guideCurveProfileUID>
+                      <fromGuideCurveUID>D150_Fuselage_1_Segment2_guide0</fromGuideCurveUID>
+                      <toRelativeCircumference>0</toRelativeCircumference>
+                    </guideCurve>
+                    <guideCurve uID="D150_Fuselage_1_Segment3_guide1">
+                      <name>D150_Fuselage_1_Segment3_guide1</name>
+                      <guideCurveProfileUID>guideCurveProfileFuselage</guideCurveProfileUID>
+                      <fromGuideCurveUID>D150_Fuselage_1_Segment2_guide1</fromGuideCurveUID>
+                      <toRelativeCircumference>0.333</toRelativeCircumference>
+                    </guideCurve>
+                    <guideCurve uID="D150_Fuselage_1_Segment3_guide2">
+                      <name>D150_Fuselage_1_Segment3_guide2</name>
+                      <guideCurveProfileUID>guideCurveProfileFuselage</guideCurveProfileUID>
+                      <fromGuideCurveUID>D150_Fuselage_1_Segment2_guide2</fromGuideCurveUID>
+                      <toRelativeCircumference>0.666</toRelativeCircumference>
+                    </guideCurve>
+                    <guideCurve uID="D150_Fuselage_1_Segment3_guide3">
+                      <name>D150_Fuselage_1_Segment3_guide3</name>
+                      <guideCurveProfileUID>guideCurveProfileFuselage</guideCurveProfileUID>
+                      <fromGuideCurveUID>D150_Fuselage_1_Segment2_guide3</fromGuideCurveUID>
+                      <toRelativeCircumference>1</toRelativeCircumference>
+                    </guideCurve>
+                </guideCurves>
+                <toElementUID>D150_Fuselage_1Section3IDElement1</toElementUID>
+              </segment>
+            </segments>
+          </fuselage>
+        </fuselages>
+        <wings>
+          <wing uID="Wing" symmetry="x-z-plane">
+            <name>Wing</name>
+            <parentUID>SimpleFuselage</parentUID>
+            <description>This wing has been generated to test CATIA2CPACS.</description>
+            <transformation uID="Wing_transformation1">
+              <scaling uID="Wing_transformation1_scaling1">
+                <x>1</x>
+                <y>1</y>
+                <z>1</z>
+              </scaling>
+              <rotation uID="Wing_transformation1_rotation1">
+                <x>0</x>
+                <y>0</y>
+                <z>0</z>
+              </rotation>
+              <translation refType="absGlobal" uID="Wing_transformation1_translation1">
+                <x>0</x>
+                <y>0</y>
+                <z>0</z>
+              </translation>
+            </transformation>
+            <sections>
+              <section uID="Cpacs2Test_Wing_Sec1">
+                <name>Cpacs2Test - Wing Section 1</name>
+                <description>Cpacs2Test - Wing Section 1</description>
+                <transformation uID="Cpacs2Test_Wing_Sec1_transformation1">
+                  <scaling uID="Cpacs2Test_Wing_Sec1_transformation1_scaling1">
+                    <x>1</x>
+                    <y>1</y>
+                    <z>1</z>
+                  </scaling>
+                  <rotation uID="Cpacs2Test_Wing_Sec1_transformation1_rotation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec1_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="Cpacs2Test_Wing_Sec1_El1">
+                    <name>Cpacs2Test - Wing Section 1 Main Element</name>
+                    <description>Cpacs2Test - Wing Section 1 Main Element</description>
+                    <airfoilUID>NACA0012</airfoilUID>
+                    <transformation uID="Cpacs2Test_Wing_Sec1_El1_transformation1">
+                      <scaling uID="Cpacs2Test_Wing_Sec1_El1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="Cpacs2Test_Wing_Sec1_El1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec1_El1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="Cpacs2Test_Wing_Sec2">
+                <name>Cpacs2Test - Wing Section 2</name>
+                <description>Cpacs2Test - Wing Section 2</description>
+                <transformation uID="Cpacs2Test_Wing_Sec2_transformation1">
+                  <scaling uID="Cpacs2Test_Wing_Sec2_transformation1_scaling1">
+                    <x>1</x>
+                    <y>1</y>
+                    <z>1</z>
+                  </scaling>
+                  <rotation uID="Cpacs2Test_Wing_Sec2_transformation1_rotation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec2_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="Cpacs2Test_Wing_Sec2_El1">
+                    <name>Cpacs2Test - Wing Section 2 Main Element</name>
+                    <description>Cpacs2Test - Wing Section 2 Main Element</description>
+                    <airfoilUID>NACA0012</airfoilUID>
+                    <transformation uID="Cpacs2Test_Wing_Sec2_El1_transformation1">
+                      <scaling uID="Cpacs2Test_Wing_Sec2_El1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="Cpacs2Test_Wing_Sec2_El1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec2_El1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="Cpacs2Test_Wing_Sec3">
+                <name>Cpacs2Test - Wing Section 3</name>
+                <description>Cpacs2Test - Wing Section 3</description>
+                <transformation uID="Cpacs2Test_Wing_Sec3_transformation1">
+                  <scaling uID="Cpacs2Test_Wing_Sec3_transformation1_scaling1">
+                    <x>1</x>
+                    <y>1</y>
+                    <z>1</z>
+                  </scaling>
+                  <rotation uID="Cpacs2Test_Wing_Sec3_transformation1_rotation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec3_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="Cpacs2Test_Wing_Sec3_El1">
+                    <name>Cpacs2Test - Wing Section 3 Main Element</name>
+                    <description>Cpacs2Test - Wing Section 3 Main Element</description>
+                    <airfoilUID>NACA0012</airfoilUID>
+                    <transformation uID="Cpacs2Test_Wing_Sec3_El1_transformation1">
+                      <scaling uID="Cpacs2Test_Wing_Sec3_El1_transformation1_scaling1">
+                        <x>0.5</x>
+                        <y>0.5</y>
+                        <z>0.5</z>
+                      </scaling>
+                      <rotation uID="Cpacs2Test_Wing_Sec3_El1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec3_El1_transformation1_translation1">
+                        <x>0.5</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+            </sections>
+            <positionings>
+              <positioning uID="Wing_positioning1">
+                <name>Cpacs2Test - Wing Section 1 Positioning</name>
+                <description>Cpacs2Test - Wing Section 1 Positioning</description>
+                <length>0</length>
+                <sweepAngle>0</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <toSectionUID>Cpacs2Test_Wing_Sec1</toSectionUID>
+              </positioning>
+              <positioning uID="Wing_positioning2">
+                <name>Cpacs2Test - Wing Section 2 Positioning</name>
+                <description>Cpacs2Test - Wing Section 2 Positioning</description>
+                <length>1</length>
+                <sweepAngle>0</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <fromSectionUID>Cpacs2Test_Wing_Sec1</fromSectionUID>
+                <toSectionUID>Cpacs2Test_Wing_Sec2</toSectionUID>
+              </positioning>
+              <positioning uID="Wing_positioning3">
+                <name>Cpacs2Test - Wing Section 3 Positioning</name>
+                <description>Cpacs2Test - Wing Section 3 Positioning</description>
+                <length>1</length>
+                <sweepAngle>0</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <fromSectionUID>Cpacs2Test_Wing_Sec2</fromSectionUID>
+                <toSectionUID>Cpacs2Test_Wing_Sec3</toSectionUID>
+              </positioning>
+            </positionings>
+            <segments>
+              <segment uID="Cpacs2Test_Wing_Seg_1_2">
+                <name>Fuselage Segment from Cpacs2Test - Wing Section 1 Main Element to Cpacs2Test - Wing Section 2 Main Element</name>
+                <description>Fuselage Segment from Cpacs2Test - Wing Section 1 Main Element to Cpacs2Test - Wing Section 2 Main Element</description>
+                <fromElementUID>Cpacs2Test_Wing_Sec1_El1</fromElementUID>
+                <toElementUID>Cpacs2Test_Wing_Sec2_El1</toElementUID>
+              </segment>
+              <segment uID="Cpacs2Test_Wing_Seg_2_3">
+                <name>Fuselage Segment from Cpacs2Test - Wing Section 2 Main Element to Cpacs2Test - Wing Section 3 Main Element</name>
+                <description>Fuselage Segment from Cpacs2Test - Wing Section 2 Main Element to Cpacs2Test - Wing Section 3 Main Element</description>
+                <fromElementUID>Cpacs2Test_Wing_Sec2_El1</fromElementUID>
+                <toElementUID>Cpacs2Test_Wing_Sec3_El1</toElementUID>
+              </segment>
+            </segments>
+            <componentSegments>
+              <componentSegment uID="WING_CS1">
+                <name>Wing_CS1</name>
+                <fromElementUID>Cpacs2Test_Wing_Sec1_El1</fromElementUID>
+                <toElementUID>Cpacs2Test_Wing_Sec3_El1</toElementUID>
+                <structure>
+                  <upperShell uID="WING_CS1_upperShell1">
+                    <skin>
+                      <material>
+                        <materialUID>MySkinMat</materialUID>
+                        <thickness>0.0</thickness>
+                      </material>
+                    </skin>
+                    <cells>
+                      <cell uID="WING_CS1_CELL1">
+                        <skin>
+                          <material>
+                            <materialUID>MyCellMat</materialUID>
+                            <thickness>0.0</thickness>
+                          </material>
+                        </skin>
+                        <positioningLeadingEdge>
+                          <xsi1>0.8</xsi1>
+                          <xsi2>0.8</xsi2>
+                        </positioningLeadingEdge>
+                        <positioningTrailingEdge>
+                          <xsi1>1.0</xsi1>
+                          <xsi2>1.0</xsi2>
+                        </positioningTrailingEdge>
+                        <positioningInnerBorder>
+                          <eta1>
+                            <eta>0</eta>
+                            <referenceUID>WING_CS1</referenceUID>
+                          </eta1>
+                          <eta2>
+                            <eta>0</eta>
+                            <referenceUID>WING_CS1</referenceUID>
+                          </eta2>
+                        </positioningInnerBorder>
+                        <positioningOuterBorder>
+                          <eta1>
+                            <eta>0.5</eta>
+                            <referenceUID>WING_CS1</referenceUID>
+                          </eta1>
+                          <eta2>
+                            <eta>0.5</eta>
+                            <referenceUID>WING_CS1</referenceUID>
+                          </eta2>
+                        </positioningOuterBorder>
+                      </cell>
+                    </cells>
+                  </upperShell>
+                  <lowerShell uID="WING_CS1_lowerShell1">
+                    <skin>
+                      <material>
+                        <materialUID>MySkinMat</materialUID>
+                      </material>
+                    </skin>
+                  </lowerShell>
+                </structure>
+              </componentSegment>
+            </componentSegments>
+          </wing>
+        </wings>
+      </model>
+    </aircraft>
+    <profiles>
+      <wingAirfoils>
+        <wingAirfoil uID="NACA0012">
+          <name>NACA0.00.00.12</name>
+          <description>NACA 4 Series Profile</description>
+          <pointList>
+            <x mapType="vector">1.0;0.9875;0.975;0.9625;0.95;0.9375;0.925;0.9125;0.9;0.8875;0.875;0.8625;0.85;0.8375;0.825;0.8125;0.8;0.7875;0.775;0.7625;0.75;0.7375;0.725;0.7125;0.7;0.6875;0.675;0.6625;0.65;0.6375;0.625;0.6125;0.6;0.5875;0.575;0.5625;0.55;0.5375;0.525;0.5125;0.5;0.4875;0.475;0.4625;0.45;0.4375;0.425;0.4125;0.4;0.3875;0.375;0.3625;0.35;0.3375;0.325;0.3125;0.3;0.2875;0.275;0.2625;0.25;0.2375;0.225;0.2125;0.2;0.1875;0.175;0.1625;0.15;0.1375;0.125;0.1125;0.1;0.0875;0.075;0.0625;0.05;0.0375;0.025;0.0125;0.0;0.0125;0.025;0.0375;0.05;0.0625;0.075;0.0875;0.1;0.1125;0.125;0.1375;0.15;0.1625;0.175;0.1875;0.2;0.2125;0.225;0.2375;0.25;0.2625;0.275;0.2875;0.3;0.3125;0.325;0.3375;0.35;0.3625;0.375;0.3875;0.4;0.4125;0.425;0.4375;0.45;0.4625;0.475;0.4875;0.5;0.5125;0.525;0.5375;0.55;0.5625;0.575;0.5875;0.6;0.6125;0.625;0.6375;0.65;0.6625;0.675;0.6875;0.7;0.7125;0.725;0.7375;0.75;0.7625;0.775;0.7875;0.8;0.8125;0.825;0.8375;0.85;0.8625;0.875;0.8875;0.9;0.9125;0.925;0.9375;0.95;0.9625;0.975;0.9875;1.0</x>
+            <y mapType="vector">0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0</y>
+            <z mapType="vector">-0.00126;-0.0030004180415;-0.00471438572941;-0.00640256842113;-0.00806559133343;-0.00970403933653;-0.0113184567357;-0.0129093470398;-0.0144771727147;-0.0160223549226;-0.0175452732434;-0.0190462653789;-0.0205256268372;-0.0219836105968;-0.0234204267471;-0.024836242105;-0.0262311798047;-0.0276053188583;-0.0289586936852;-0.0302912936071;-0.0316030623052;-0.0328938972373;-0.0341636490097;-0.0354121207001;-0.0366390671268;-0.0378441940595;-0.0390271573644;-0.0401875620783;-0.0413249614032;-0.042438855614;-0.043528690869;-0.0445938579126;-0.0456336906587;-0.04664746464;-0.0476343953088;-0.0485936361694;-0.0495242767241;-0.0504253402064;-0.0512957810767;-0.0521344822472;-0.0529402520006;-0.0537118205596;-0.0544478362583;-0.0551468612564;-0.0558073667285;-0.0564277274483;-0.0570062156697;-0.0575409941929;-0.0580301084765;-0.0584714776309;-0.0588628840933;-0.059201961739;-0.0594861821311;-0.0597128385384;-0.059879027262;-0.0599816256958;-0.060017266394;-0.059982306219;-0.05987278938;-0.0596844028137;-0.059412421875;-0.059051643633;-0.0585963041308;-0.0580399746271;-0.0573754299024;-0.0565944788455;-0.0556877432118;-0.054644363746;-0.0534516022043;-0.0520942903127;-0.0505540468987;-0.0488081315259;-0.0468277042382;-0.0445750655553;-0.0419990347204;-0.0390266537476;-0.0355468568262;-0.0313738751622;-0.0261471986426;-0.0189390266528;0.0;0.0189390266528;0.0261471986426;0.0313738751622;0.0355468568262;0.0390266537476;0.0419990347204;0.0445750655553;0.0468277042382;0.0488081315259;0.0505540468987;0.0520942903127;0.0534516022043;0.054644363746;0.0556877432118;0.0565944788455;0.0573754299024;0.0580399746271;0.0585963041308;0.059051643633;0.059412421875;0.0596844028137;0.05987278938;0.059982306219;0.060017266394;0.0599816256958;0.059879027262;0.0597128385384;0.0594861821311;0.059201961739;0.0588628840933;0.0584714776309;0.0580301084765;0.0575409941929;0.0570062156697;0.0564277274483;0.0558073667285;0.0551468612564;0.0544478362583;0.0537118205596;0.0529402520006;0.0521344822472;0.0512957810767;0.0504253402064;0.0495242767241;0.0485936361694;0.0476343953088;0.04664746464;0.0456336906587;0.0445938579126;0.043528690869;0.042438855614;0.0413249614032;0.0401875620783;0.0390271573644;0.0378441940595;0.0366390671268;0.0354121207001;0.0341636490097;0.0328938972373;0.0316030623052;0.0302912936071;0.0289586936852;0.0276053188583;0.0262311798047;0.024836242105;0.0234204267471;0.0219836105968;0.0205256268372;0.0190462653789;0.0175452732434;0.0160223549226;0.0144771727147;0.0129093470398;0.0113184567357;0.00970403933653;0.00806559133343;0.00640256842113;0.00471438572941;0.0030004180415;0.00126</z>
+          </pointList>
+        </wingAirfoil>
+      </wingAirfoils>
+      <fuselageProfiles>
+        <fuselageProfile uID="fuselageCircleProfileuID">
+          <name>Circle</name>
+          <description>Profile build up from set of Points on Circle where may Dimensions are 1..-1</description>
+          <pointList>
+            <x mapType="vector">0.0;0.0;0.0;0.0;0.0</x>
+            <y mapType="vector">0.0;1.0;0.0;-1.0;0.0</y>
+            <z mapType="vector">1.0;0.0;-1.0;0.0;1.0</z>
+          </pointList>
+        </fuselageProfile>
+        <fuselageProfile uID="fuselageRectangleProfileuID">
+          <name>Rectangle</name>
+          <description>Standard Profile Type Rectangle</description>
+          <standardProfile>
+            <rectangle>
+                <heightToWidthRatio>0.5</heightToWidthRatio>
+            </rectangle>
+          </standardProfile>
+        </fuselageProfile>
+          <fuselageProfile uID="fuselageRectangle1ProfileuID">
+          <name>Rectangle1</name>
+          <description>Standard Profile Type Rectangle</description>
+          <standardProfile>
+            <rectangle>
+                <heightToWidthRatio>0.5</heightToWidthRatio>
+                <cornerRadius>0.14</cornerRadius>
+            </rectangle>
+          </standardProfile>
+        </fuselageProfile>
+      </fuselageProfiles>
+      <guideCurves>
+        <guideCurveProfile uID="guideCurveProfileFuselage">
+          <name>GuideCurveProfileFuselage</name>
+          <pointList>
+            <rX mapType="vector">0.0</rX>
+            <rY mapType="vector">0.5</rY>
+            <rZ mapType="vector">0.0</rZ>
+          </pointList>
+        </guideCurveProfile>
+      </guideCurves>
+    </profiles>
+  </vehicles>
+  <toolspecific>
+    <cFD>
+      <farField>
+        <type>halfCube</type>
+        <referenceLength>10.0</referenceLength>
+        <multiplier>1.</multiplier>
+      </farField>
+    </cFD>
+  </toolspecific>
+</cpacs>
diff --git a/tests/unittests/TestData/simpletest_standard_profile_rectangle_circle_kink.cpacs.xml b/tests/unittests/TestData/simpletest_standard_profile_rectangle_circle_kink.cpacs.xml
new file mode 100644
index 000000000..a70eaf189
--- /dev/null
+++ b/tests/unittests/TestData/simpletest_standard_profile_rectangle_circle_kink.cpacs.xml
@@ -0,0 +1,734 @@
+<?xml version="1.0" encoding="utf-8"?>
+<cpacs xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="http://cpacs.googlecode.com/files/CPACS_21_Schema.xsd">
+  <header>
+    <name>Cpacs2Test</name>
+    <description>Simple Wing with 4 guide curves for testing</description>
+    <creator>Martin Siggel</creator>
+    <timestamp>2020-10-12T12:26:00</timestamp>
+    <version>0.5.0</version>
+    <cpacsVersion>3.2</cpacsVersion>
+    <updates>
+      <update>
+        <modification>Converted to CPACS 3.2 using cpacs2to3</modification>
+        <creator>cpacs2to3</creator>
+        <timestamp>2021-04-23T18:02:03</timestamp>
+        <version>0.5.0</version>
+        <cpacsVersion>3.2</cpacsVersion>
+      </update>
+    </updates>
+  </header>
+  <vehicles>
+    <aircraft>
+      <model uID="Cpacs2Test">
+        <name>Cpacs2Test</name>
+        <reference>
+          <area>1</area>
+          <length>1</length>
+          <point uID="Cpacs2Test_point1">
+            <x>0</x>
+            <y>0</y>
+            <z>0</z>
+          </point>
+        </reference>
+        <fuselages>
+          <fuselage uID="SimpleFuselage">
+            <name>name</name>
+            <description>description</description>
+            <transformation uID="SimpleFuselage_transformation1">
+              <scaling uID="SimpleFuselage_transformation1_scaling1">
+                <x>1.0</x>
+                <y>0.5</y>
+                <z>0.5</z>
+              </scaling>
+              <rotation uID="SimpleFuselage_transformation1_rotation1">
+                <x>0.0</x>
+                <y>0.0</y>
+                <z>0.0</z>
+              </rotation>
+              <translation refType="absLocal" uID="SimpleFuselage_transformation1_translation1">
+                <x>0.0</x>
+                <y>0.0</y>
+                <z>0.0</z>
+              </translation>
+            </transformation>
+            <sections>
+              <section uID="D150_Fuselage_1Section1ID">
+                <name>D150_Fuselage_1Section1</name>
+                <transformation uID="D150_Fuselage_1Section1ID_transformation1">
+                  <scaling uID="D150_Fuselage_1Section1ID_transformation1_scaling1">
+                    <x>1.0</x>
+                    <y>1.0</y>
+                    <z>1.0</z>
+                  </scaling>
+                  <rotation uID="D150_Fuselage_1Section1ID_transformation1_rotation1">
+                    <x>0.0</x>
+                    <y>0.0</y>
+                    <z>0.0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="D150_Fuselage_1Section1ID_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="D150_Fuselage_1Section1IDElement1">
+                    <name>D150_Fuselage_1Section1</name>
+                    <profileUID>fuselageCircle1ProfileuID</profileUID>
+                    <transformation uID="D150_Fuselage_1Section1IDElement1_transformation1">
+                      <scaling uID="D150_Fuselage_1Section1IDElement1_transformation1_scaling1">
+                        <x>1.0</x>
+                        <y>1.0</y>
+                        <z>1.0</z>
+                      </scaling>
+                      <rotation uID="D150_Fuselage_1Section1IDElement1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="D150_Fuselage_1Section1IDElement1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="D150_Fuselage_1Section2ID">
+                <name>D150_Fuselage_1Section2</name>
+                <transformation uID="D150_Fuselage_1Section2ID_transformation1">
+                  <scaling uID="D150_Fuselage_1Section2ID_transformation1_scaling1">
+                    <x>1.0</x>
+                    <y>1.0</y>
+                    <z>1.0</z>
+                  </scaling>
+                  <rotation uID="D150_Fuselage_1Section2ID_transformation1_rotation1">
+                    <x>0.0</x>
+                    <y>0.0</y>
+                    <z>0.0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="D150_Fuselage_1Section2ID_transformation1_translation1">
+                    <x>0.01</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="D150_Fuselage_1Section2IDElement1">
+                    <name>D150_Fuselage_1Section2</name>
+                    <profileUID>fuselageCircleProfileuID</profileUID>
+                    <transformation uID="D150_Fuselage_1Section2IDElement1_transformation1">
+                      <scaling uID="D150_Fuselage_1Section2IDElement1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="D150_Fuselage_1Section2IDElement1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="D150_Fuselage_1Section2IDElement1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="D150_Fuselage_1Section3ID">
+                <name>D150_Fuselage_1Section3</name>
+                <transformation uID="D150_Fuselage_1Section3ID_transformation1">
+                  <scaling uID="D150_Fuselage_1Section3ID_transformation1_scaling1">
+                    <x>1.0</x>
+                    <y>3.0</y>
+                    <z>3.0</z>
+                  </scaling>
+                  <rotation uID="D150_Fuselage_1Section3ID_transformation1_rotation1">
+                    <x>0.0</x>
+                    <y>0.0</y>
+                    <z>0.0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="D150_Fuselage_1Section3ID_transformation1_translation1">
+                    <x>1</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="D150_Fuselage_1Section3IDElement1">
+                    <name>D150_Fuselage_1Section3</name>
+                    <profileUID>fuselageRectangleProfileuID</profileUID>
+                    <transformation uID="D150_Fuselage_1Section3IDElement1_transformation1">
+                      <scaling uID="D150_Fuselage_1Section3IDElement1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="D150_Fuselage_1Section3IDElement1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="D150_Fuselage_1Section3IDElement1_transformation1_translation1">
+                        <x>0.5</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="D150_Fuselage_1Section4ID">
+                <name>D150_Fuselage_1Section3</name>
+                <transformation uID="D150_Fuselage_1Section4ID_transformation1">
+                  <scaling uID="D150_Fuselage_1Section4ID_transformation1_scaling1">
+                    <x>1.0</x>
+                    <y>1.0</y>
+                    <z>1.0</z>
+                  </scaling>
+                  <rotation uID="D150_Fuselage_1Section4ID_transformation1_rotation1">
+                    <x>0.0</x>
+                    <y>0.0</y>
+                    <z>0.0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="D150_Fuselage_1Section4ID_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="D150_Fuselage_1Section4IDElement1">
+                    <name>D150_Fuselage_1Section3</name>
+                    <profileUID>fuselageRectangle1ProfileuID</profileUID>
+                    <transformation uID="D150_Fuselage_1Section4IDElement1_transformation1">
+                      <scaling uID="D150_Fuselage_1Section4IDElement1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="D150_Fuselage_1Section4IDElement1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="D150_Fuselage_1Section4IDElement1_transformation1_translation1">
+                        <x>0.9</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+            </sections>
+            <positionings>
+              <positioning uID="D150_Fuselage_1Positioning1ID">
+                <name>D150_Fuselage_1Positioning1</name>
+                <length>-0.5</length>
+                <sweepAngle>90</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <toSectionUID>D150_Fuselage_1Section1ID</toSectionUID>
+              </positioning>
+              <positioning uID="D150_Fuselage_1Positioning3ID">
+                <name>D150_Fuselage_1Positioning3</name>
+                <length>2</length>
+                <sweepAngle>90</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <fromSectionUID>D150_Fuselage_1Section1ID</fromSectionUID>
+                <toSectionUID>D150_Fuselage_1Section4ID</toSectionUID>
+              </positioning>
+            </positionings>
+            <segments>
+              <segment uID="segmentD150_Fuselage_1Segment2ID">
+                <name>D150_Fuselage_1Segment2</name>
+                <fromElementUID>D150_Fuselage_1Section1IDElement1</fromElementUID>
+                <toElementUID>D150_Fuselage_1Section2IDElement1</toElementUID>
+              </segment>
+              <segment uID="segmentD150_Fuselage_1Segment3ID">
+                <name>D150_Fuselage_1Segment3</name>
+                <fromElementUID>D150_Fuselage_1Section2IDElement1</fromElementUID>
+                <toElementUID>D150_Fuselage_1Section3IDElement1</toElementUID>
+              </segment>
+                <segment uID="segmentD150_Fuselage_1Segment4ID">
+                <name>D150_Fuselage_1Segment4</name>
+                <fromElementUID>D150_Fuselage_1Section3IDElement1</fromElementUID>
+                <toElementUID>D150_Fuselage_1Section4IDElement1</toElementUID>
+              </segment>
+            </segments>
+          </fuselage>
+        </fuselages>
+        <wings>
+          <wing uID="Wing" symmetry="x-z-plane">
+            <name>Wing</name>
+            <parentUID>SimpleFuselage</parentUID>
+            <description>This wing has been generated to test CATIA2CPACS.</description>
+            <transformation uID="Wing_transformation1">
+              <scaling uID="Wing_transformation1_scaling1">
+                <x>1</x>
+                <y>1</y>
+                <z>1</z>
+              </scaling>
+              <rotation uID="Wing_transformation1_rotation1">
+                <x>0</x>
+                <y>0</y>
+                <z>0</z>
+              </rotation>
+              <translation refType="absGlobal" uID="Wing_transformation1_translation1">
+                <x>0</x>
+                <y>0</y>
+                <z>0</z>
+              </translation>
+            </transformation>
+            <sections>
+              <section uID="Cpacs2Test_Wing_Sec1">
+                <name>Cpacs2Test - Wing Section 1</name>
+                <description>Cpacs2Test - Wing Section 1</description>
+                <transformation uID="Cpacs2Test_Wing_Sec1_transformation1">
+                  <scaling uID="Cpacs2Test_Wing_Sec1_transformation1_scaling1">
+                    <x>1</x>
+                    <y>1</y>
+                    <z>2.5</z>
+                  </scaling>
+                  <rotation uID="Cpacs2Test_Wing_Sec1_transformation1_rotation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec1_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="Cpacs2Test_Wing_Sec1_El1">
+                    <name>Cpacs2Test - Wing Section 1 Main Element</name>
+                    <description>Cpacs2Test - Wing Section 1 Main Element</description>
+                    <airfoilUID>NACA0012</airfoilUID>
+                    <transformation uID="Cpacs2Test_Wing_Sec1_El1_transformation1">
+                      <scaling uID="Cpacs2Test_Wing_Sec1_El1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="Cpacs2Test_Wing_Sec1_El1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec1_El1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="Cpacs2Test_Wing_Sec2">
+                <name>Cpacs2Test - Wing Section 2</name>
+                <description>Cpacs2Test - Wing Section 2</description>
+                <transformation uID="Cpacs2Test_Wing_Sec2_transformation1">
+                  <scaling uID="Cpacs2Test_Wing_Sec2_transformation1_scaling1">
+                    <x>1</x>
+                    <y>2</y>
+                    <z>1</z>
+                  </scaling>
+                  <rotation uID="Cpacs2Test_Wing_Sec2_transformation1_rotation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec2_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="Cpacs2Test_Wing_Sec2_El1">
+                    <name>Cpacs2Test - Wing Section 2 Main Element</name>
+                    <description>Cpacs2Test - Wing Section 2 Main Element</description>
+                    <airfoilUID>NACA0012</airfoilUID>
+                    <transformation uID="Cpacs2Test_Wing_Sec2_El1_transformation1">
+                      <scaling uID="Cpacs2Test_Wing_Sec2_El1_transformation1_scaling1">
+                        <x>1</x>
+                        <y>1</y>
+                        <z>1</z>
+                      </scaling>
+                      <rotation uID="Cpacs2Test_Wing_Sec2_El1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec2_El1_transformation1_translation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+              <section uID="Cpacs2Test_Wing_Sec3">
+                <name>Cpacs2Test - Wing Section 3</name>
+                <description>Cpacs2Test - Wing Section 3</description>
+                <transformation uID="Cpacs2Test_Wing_Sec3_transformation1">
+                  <scaling uID="Cpacs2Test_Wing_Sec3_transformation1_scaling1">
+                    <x>1</x>
+                    <y>1</y>
+                    <z>0.5</z>
+                  </scaling>
+                  <rotation uID="Cpacs2Test_Wing_Sec3_transformation1_rotation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </rotation>
+                  <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec3_transformation1_translation1">
+                    <x>0</x>
+                    <y>0</y>
+                    <z>0</z>
+                  </translation>
+                </transformation>
+                <elements>
+                  <element uID="Cpacs2Test_Wing_Sec3_El1">
+                    <name>Cpacs2Test - Wing Section 3 Main Element</name>
+                    <description>Cpacs2Test - Wing Section 3 Main Element</description>
+                    <airfoilUID>NACA0012</airfoilUID>
+                    <transformation uID="Cpacs2Test_Wing_Sec3_El1_transformation1">
+                      <scaling uID="Cpacs2Test_Wing_Sec3_El1_transformation1_scaling1">
+                        <x>0.5</x>
+                        <y>0.5</y>
+                        <z>0.5</z>
+                      </scaling>
+                      <rotation uID="Cpacs2Test_Wing_Sec3_El1_transformation1_rotation1">
+                        <x>0</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </rotation>
+                      <translation refType="absLocal" uID="Cpacs2Test_Wing_Sec3_El1_transformation1_translation1">
+                        <x>0.5</x>
+                        <y>0</y>
+                        <z>0</z>
+                      </translation>
+                    </transformation>
+                  </element>
+                </elements>
+              </section>
+            </sections>
+            <positionings>
+              <positioning uID="Wing_positioning1">
+                <name>Cpacs2Test - Wing Section 1 Positioning</name>
+                <description>Cpacs2Test - Wing Section 1 Positioning</description>
+                <length>0</length>
+                <sweepAngle>0</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <toSectionUID>Cpacs2Test_Wing_Sec1</toSectionUID>
+              </positioning>
+              <positioning uID="Wing_positioning2">
+                <name>Cpacs2Test - Wing Section 2 Positioning</name>
+                <description>Cpacs2Test - Wing Section 2 Positioning</description>
+                <length>0.8</length>
+                <sweepAngle>0</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <fromSectionUID>Cpacs2Test_Wing_Sec1</fromSectionUID>
+                <toSectionUID>Cpacs2Test_Wing_Sec2</toSectionUID>
+              </positioning>
+              <positioning uID="Wing_positioning3">
+                <name>Cpacs2Test - Wing Section 3 Positioning</name>
+                <description>Cpacs2Test - Wing Section 3 Positioning</description>
+                <length>1</length>
+                <sweepAngle>0</sweepAngle>
+                <dihedralAngle>0</dihedralAngle>
+                <fromSectionUID>Cpacs2Test_Wing_Sec2</fromSectionUID>
+                <toSectionUID>Cpacs2Test_Wing_Sec3</toSectionUID>
+              </positioning>
+            </positionings>
+            <segments>
+              <segment uID="Cpacs2Test_Wing_Seg_1_2">
+                <name>Fuselage Segment from Cpacs2Test - Wing Section 1 Main Element to Cpacs2Test - Wing Section 2 Main Element</name>
+                <description>Fuselage Segment from Cpacs2Test - Wing Section 1 Main Element to Cpacs2Test - Wing Section 2 Main Element</description>
+                <fromElementUID>Cpacs2Test_Wing_Sec1_El1</fromElementUID>
+                <toElementUID>Cpacs2Test_Wing_Sec2_El1</toElementUID>
+                <guideCurves>
+                  <guideCurve uID="Wing_Seg_1_2_GuideCurve_Upper">
+                    <name>Leading Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </name>
+                    <description>Leading Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </description>
+                    <guideCurveProfileUID>S1_UPPER_GUIDE</guideCurveProfileUID>
+                    <fromRelativeCircumference>0.5</fromRelativeCircumference>
+                    <toRelativeCircumference>0.5    </toRelativeCircumference>
+                  </guideCurve>
+                  <guideCurve uID="Wing_Seg_1_2_GuideCurve_TrailingEdgeLower">
+                    <name>Lower Trailing Edge GuideCurve from GuideCurveModel - Wing Section 1 Main Element to GuideCurveModel - Wing Section 2 Main Element </name>
+                    <description>Lower Trailing Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </description>
+                    <guideCurveProfileUID>S1_TE_LOWER_GUIDE</guideCurveProfileUID>
+                    <fromRelativeCircumference>-1.0</fromRelativeCircumference>
+                    <toRelativeCircumference>-1.0</toRelativeCircumference>
+                  </guideCurve>
+                  <guideCurve uID="Wing_Seg_1_2_GuideCurve_LeadingEdge">
+                    <name>Leading Edge GuideCurve from GuideCurveModel - Wing Section 1 Main Element to GuideCurveModel - Wing Section 2 Main Element </name>
+                    <description>Leading Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 2 Main Element </description>
+                    <guideCurveProfileUID>S1_LE_GUIDE</guideCurveProfileUID>
+                    <fromRelativeCircumference>0.0</fromRelativeCircumference>
+                    <toRelativeCircumference>0.0</toRelativeCircumference>
+                  </guideCurve>
+                  <guideCurve uID="Wing_Seg_1_2_GuideCurve_TrailingEdgeUpper">
+                    <name>Upper Trailing Edge GuideCurve from GuideCurveModel - Wing Section 1 Main Element to GuideCurveModel - Wing Section 2 Main Element </name>
+                    <description>Upper Trailing Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 2 Main Element </description>
+                    <guideCurveProfileUID>S1_TE_UPPER_GUIDE</guideCurveProfileUID>
+                    <fromRelativeCircumference>1.0</fromRelativeCircumference>
+                    <toRelativeCircumference>1.0</toRelativeCircumference>
+                  </guideCurve>
+                </guideCurves>
+              </segment>
+              <segment uID="Cpacs2Test_Wing_Seg_2_3">
+                <name>Fuselage Segment from Cpacs2Test - Wing Section 2 Main Element to Cpacs2Test - Wing Section 3 Main Element</name>
+                <description>Fuselage Segment from Cpacs2Test - Wing Section 2 Main Element to Cpacs2Test - Wing Section 3 Main Element</description>
+                <fromElementUID>Cpacs2Test_Wing_Sec2_El1</fromElementUID>
+                <toElementUID>Cpacs2Test_Wing_Sec3_El1</toElementUID>
+                <guideCurves>
+                  <guideCurve uID="Wing_Seg_2_3_GuideCurve_Upper">
+                    <name>Leading Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </name>
+                    <description>Leading Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </description>
+                    <guideCurveProfileUID>S2_UPPER_GUIDE</guideCurveProfileUID>
+                    <continuity>C1 from previous</continuity>
+                    <fromGuideCurveUID>Wing_Seg_1_2_GuideCurve_Upper</fromGuideCurveUID>
+                    <toRelativeCircumference>0.5</toRelativeCircumference>
+                  </guideCurve>
+                  <guideCurve uID="Wing_Seg_2_3_GuideCurve_TrailingEdgeLower">
+                    <name>Lower Trailing Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </name>
+                    <description>Lower Trailing Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </description>
+                    <guideCurveProfileUID>S2_TE_LOWER_GUIDE</guideCurveProfileUID>
+                    <fromGuideCurveUID>Wing_Seg_1_2_GuideCurve_TrailingEdgeLower</fromGuideCurveUID>
+                    <toRelativeCircumference>-1.0</toRelativeCircumference>
+                  </guideCurve>
+                  <guideCurve uID="Wing_Seg_2_3_GuideCurve_TrailingEdgeUpper">
+                    <name>Upper Trailing Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </name>
+                    <description>Upper Trailing Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </description>
+                    <guideCurveProfileUID>S2_TE_UPPER_GUIDE</guideCurveProfileUID>
+                    <fromGuideCurveUID>Wing_Seg_1_2_GuideCurve_TrailingEdgeUpper</fromGuideCurveUID>
+                    <toRelativeCircumference>1.0</toRelativeCircumference>
+                  </guideCurve>
+                  <guideCurve uID="Wing_Seg_2_3_GuideCurve_LeadingEdge">
+                    <name>Leading Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </name>
+                    <description>Leading Edge GuideCurve from GuideCurveModel - Wing Section 2 Main Element to GuideCurveModel - Wing Section 3 Main Element </description>
+                    <guideCurveProfileUID>S2_LE_GUIDE</guideCurveProfileUID>
+                    <continuity>C1 from previous</continuity>
+                    <fromGuideCurveUID>Wing_Seg_1_2_GuideCurve_LeadingEdge</fromGuideCurveUID>
+                    <toRelativeCircumference>0.0</toRelativeCircumference>
+                  </guideCurve>
+                </guideCurves>
+              </segment>
+            </segments>
+            <componentSegments>
+              <componentSegment uID="WING_CS1">
+                <name>Wing_CS1</name>
+                <fromElementUID>Cpacs2Test_Wing_Sec1_El1</fromElementUID>
+                <toElementUID>Cpacs2Test_Wing_Sec3_El1</toElementUID>
+                <structure>
+                  <upperShell uID="WING_CS1_upperShell1">
+                    <skin>
+                      <material>
+                        <materialUID>MySkinMat</materialUID>
+                        <thickness>0.0</thickness>
+                      </material>
+                    </skin>
+                    <cells>
+                      <cell uID="WING_CS1_CELL1">
+                        <skin>
+                          <material>
+                            <materialUID>MyCellMat</materialUID>
+                            <thickness>0.0</thickness>
+                          </material>
+                        </skin>
+                        <positioningLeadingEdge>
+                          <xsi1>0.8</xsi1>
+                          <xsi2>0.8</xsi2>
+                        </positioningLeadingEdge>
+                        <positioningTrailingEdge>
+                          <xsi1>1.0</xsi1>
+                          <xsi2>1.0</xsi2>
+                        </positioningTrailingEdge>
+                        <positioningInnerBorder>
+                          <eta1>
+                            <eta>0</eta>
+                            <referenceUID>WING_CS1</referenceUID>
+                          </eta1>
+                          <eta2>
+                            <eta>0</eta>
+                            <referenceUID>WING_CS1</referenceUID>
+                          </eta2>
+                        </positioningInnerBorder>
+                        <positioningOuterBorder>
+                          <eta1>
+                            <eta>0.5</eta>
+                            <referenceUID>WING_CS1</referenceUID>
+                          </eta1>
+                          <eta2>
+                            <eta>0.5</eta>
+                            <referenceUID>WING_CS1</referenceUID>
+                          </eta2>
+                        </positioningOuterBorder>
+                      </cell>
+                    </cells>
+                  </upperShell>
+                  <lowerShell uID="WING_CS1_lowerShell1">
+                    <skin>
+                      <material>
+                        <materialUID>MySkinMat</materialUID>
+                      </material>
+                    </skin>
+                  </lowerShell>
+                </structure>
+              </componentSegment>
+            </componentSegments>
+          </wing>
+        </wings>
+      </model>
+    </aircraft>
+    <profiles>
+      <wingAirfoils>
+        <wingAirfoil uID="NACA0012">
+          <name>NACA0.00.00.12</name>
+          <description>NACA 4 Series Profile</description>
+          <pointList>
+            <x mapType="vector">1.0;0.9875;0.975;0.9625;0.95;0.9375;0.925;0.9125;0.9;0.8875;0.875;0.8625;0.85;0.8375;0.825;0.8125;0.8;0.7875;0.775;0.7625;0.75;0.7375;0.725;0.7125;0.7;0.6875;0.675;0.6625;0.65;0.6375;0.625;0.6125;0.6;0.5875;0.575;0.5625;0.55;0.5375;0.525;0.5125;0.5;0.4875;0.475;0.4625;0.45;0.4375;0.425;0.4125;0.4;0.3875;0.375;0.3625;0.35;0.3375;0.325;0.3125;0.3;0.2875;0.275;0.2625;0.25;0.2375;0.225;0.2125;0.2;0.1875;0.175;0.1625;0.15;0.1375;0.125;0.1125;0.1;0.0875;0.075;0.0625;0.05;0.0375;0.025;0.0125;0.0;0.0125;0.025;0.0375;0.05;0.0625;0.075;0.0875;0.1;0.1125;0.125;0.1375;0.15;0.1625;0.175;0.1875;0.2;0.2125;0.225;0.2375;0.25;0.2625;0.275;0.2875;0.3;0.3125;0.325;0.3375;0.35;0.3625;0.375;0.3875;0.4;0.4125;0.425;0.4375;0.45;0.4625;0.475;0.4875;0.5;0.5125;0.525;0.5375;0.55;0.5625;0.575;0.5875;0.6;0.6125;0.625;0.6375;0.65;0.6625;0.675;0.6875;0.7;0.7125;0.725;0.7375;0.75;0.7625;0.775;0.7875;0.8;0.8125;0.825;0.8375;0.85;0.8625;0.875;0.8875;0.9;0.9125;0.925;0.9375;0.95;0.9625;0.975;0.9875;1.0</x>
+            <y mapType="vector">0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0</y>
+            <z mapType="vector">-0.00126;-0.0030004180415;-0.00471438572941;-0.00640256842113;-0.00806559133343;-0.00970403933653;-0.0113184567357;-0.0129093470398;-0.0144771727147;-0.0160223549226;-0.0175452732434;-0.0190462653789;-0.0205256268372;-0.0219836105968;-0.0234204267471;-0.024836242105;-0.0262311798047;-0.0276053188583;-0.0289586936852;-0.0302912936071;-0.0316030623052;-0.0328938972373;-0.0341636490097;-0.0354121207001;-0.0366390671268;-0.0378441940595;-0.0390271573644;-0.0401875620783;-0.0413249614032;-0.042438855614;-0.043528690869;-0.0445938579126;-0.0456336906587;-0.04664746464;-0.0476343953088;-0.0485936361694;-0.0495242767241;-0.0504253402064;-0.0512957810767;-0.0521344822472;-0.0529402520006;-0.0537118205596;-0.0544478362583;-0.0551468612564;-0.0558073667285;-0.0564277274483;-0.0570062156697;-0.0575409941929;-0.0580301084765;-0.0584714776309;-0.0588628840933;-0.059201961739;-0.0594861821311;-0.0597128385384;-0.059879027262;-0.0599816256958;-0.060017266394;-0.059982306219;-0.05987278938;-0.0596844028137;-0.059412421875;-0.059051643633;-0.0585963041308;-0.0580399746271;-0.0573754299024;-0.0565944788455;-0.0556877432118;-0.054644363746;-0.0534516022043;-0.0520942903127;-0.0505540468987;-0.0488081315259;-0.0468277042382;-0.0445750655553;-0.0419990347204;-0.0390266537476;-0.0355468568262;-0.0313738751622;-0.0261471986426;-0.0189390266528;0.0;0.0189390266528;0.0261471986426;0.0313738751622;0.0355468568262;0.0390266537476;0.0419990347204;0.0445750655553;0.0468277042382;0.0488081315259;0.0505540468987;0.0520942903127;0.0534516022043;0.054644363746;0.0556877432118;0.0565944788455;0.0573754299024;0.0580399746271;0.0585963041308;0.059051643633;0.059412421875;0.0596844028137;0.05987278938;0.059982306219;0.060017266394;0.0599816256958;0.059879027262;0.0597128385384;0.0594861821311;0.059201961739;0.0588628840933;0.0584714776309;0.0580301084765;0.0575409941929;0.0570062156697;0.0564277274483;0.0558073667285;0.0551468612564;0.0544478362583;0.0537118205596;0.0529402520006;0.0521344822472;0.0512957810767;0.0504253402064;0.0495242767241;0.0485936361694;0.0476343953088;0.04664746464;0.0456336906587;0.0445938579126;0.043528690869;0.042438855614;0.0413249614032;0.0401875620783;0.0390271573644;0.0378441940595;0.0366390671268;0.0354121207001;0.0341636490097;0.0328938972373;0.0316030623052;0.0302912936071;0.0289586936852;0.0276053188583;0.0262311798047;0.024836242105;0.0234204267471;0.0219836105968;0.0205256268372;0.0190462653789;0.0175452732434;0.0160223549226;0.0144771727147;0.0129093470398;0.0113184567357;0.00970403933653;0.00806559133343;0.00640256842113;0.00471438572941;0.0030004180415;0.00126</z>
+          </pointList>
+        </wingAirfoil>
+      </wingAirfoils>
+      <fuselageProfiles>
+        <fuselageProfile uID="fuselageCircleProfileuID">
+          <name>Circle</name>
+          <description>Profile build up from set of Points on Circle where may Dimensions are 1..-1</description>
+          <pointList>
+            <x mapType="vector">0.0;0.0;0.0;0.0;0.0</x>
+            <y mapType="vector">0.0;1.0;0.0;-1.0;0.0</y>
+            <z mapType="vector">1.0;0.0;-1.0;0.0;1.0</z>
+          </pointList>
+        </fuselageProfile>
+        <fuselageProfile uID="fuselageCircle1ProfileuID">
+          <name>Circle1</name>
+          <description>Profile build up from set of Points on Circle where may Dimensions are 1..-1</description>
+          <pointList>
+            <x mapType="vector">0.0;0.0;0.0;0.0;0.0</x>
+            <y mapType="vector">0.0;1.0;0.0;-1.0;0.0</y>
+            <z mapType="vector">1.0;0.0;-1.0;0.0;1.0</z>
+            <kinkIndices mapType="vector">1;3</kinkIndices>
+            <parameterMap>
+              <pointIndices mapType="vector">1;3</pointIndices>
+              <paramOnCurve mapType="vector">0.25;0.75</paramOnCurve>
+            </parameterMap>
+          </pointList>
+        </fuselageProfile>
+        <fuselageProfile uID="fuselageRectangleProfileuID">
+          <name>Rectangle</name>
+          <description>Standard Profile Type Rectangle</description>
+          <standardProfile>
+            <rectangle>
+                <heightToWidthRatio>0.5</heightToWidthRatio>
+            </rectangle>
+          </standardProfile>
+        </fuselageProfile>
+          <fuselageProfile uID="fuselageRectangle1ProfileuID">
+          <name>Rectangle1</name>
+          <description>Standard Profile Type Rectangle</description>
+          <standardProfile>
+            <rectangle>
+                <heightToWidthRatio>1</heightToWidthRatio>
+                <cornerRadius>0.14</cornerRadius>
+            </rectangle>
+          </standardProfile>
+        </fuselageProfile>
+      </fuselageProfiles>
+      <guideCurves>
+        <guideCurveProfile uID="S1_TE_LOWER_GUIDE">
+          <name>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</name>
+          <description>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</description>
+          <pointList>
+            <rX mapType="vector">0;0;0</rX>
+            <rY mapType="vector">0.1;0.5;0.9</rY>
+            <rZ mapType="vector">0;0;0</rZ>
+          </pointList>
+        </guideCurveProfile>
+        <guideCurveProfile uID="S1_LE_GUIDE">
+          <name>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</name>
+          <description>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</description>
+          <pointList>
+            <rX mapType="vector">0</rX>
+            <rY mapType="vector">0.5</rY>
+            <rZ mapType="vector">0</rZ>
+          </pointList>
+        </guideCurveProfile>
+        <guideCurveProfile uID="S1_UPPER_GUIDE">
+          <name>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</name>
+          <description>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</description>
+          <pointList>
+            <rX mapType="vector">0</rX>
+            <rY mapType="vector">0.5</rY>
+            <rZ mapType="vector">0.01</rZ>
+          </pointList>
+        </guideCurveProfile>
+        <guideCurveProfile uID="S1_TE_UPPER_GUIDE">
+          <name>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</name>
+          <description>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</description>
+          <pointList>
+            <rX mapType="vector">0;0;0</rX>
+            <rY mapType="vector">0.1;0.5;0.9</rY>
+            <rZ mapType="vector">0;0;0</rZ>
+          </pointList>
+        </guideCurveProfile>
+        <guideCurveProfile uID="S2_TE_LOWER_GUIDE">
+          <name>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</name>
+          <description>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</description>
+          <pointList>
+            <rX mapType="vector">0;0;0</rX>
+            <rY mapType="vector">0.1;0.5;0.9</rY>
+            <rZ mapType="vector">0;0;0</rZ>
+          </pointList>
+        </guideCurveProfile>
+        <guideCurveProfile uID="S2_LE_GUIDE">
+          <name>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</name>
+          <description>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</description>
+          <pointList>
+            <rX mapType="vector">-0.2</rX>
+            <rY mapType="vector">0.5</rY>
+            <rZ mapType="vector">0</rZ>
+          </pointList>
+        </guideCurveProfile>
+        <guideCurveProfile uID="S2_UPPER_GUIDE">
+          <name>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</name>
+          <description>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</description>
+          <pointList>
+            <rX mapType="vector">-0.05</rX>
+            <rY mapType="vector">0.5</rY>
+            <rZ mapType="vector"> -0.03</rZ>
+          </pointList>
+        </guideCurveProfile>
+        <guideCurveProfile uID="S2_TE_UPPER_GUIDE">
+          <name>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</name>
+          <description>Linear Lower Guide Curve Profile for GuideCurveModel - Fuselage</description>
+          <pointList>
+            <rX mapType="vector">0;0;0</rX>
+            <rY mapType="vector">0.1;0.5;0.9</rY>
+            <rZ mapType="vector">0;0;0</rZ>
+          </pointList>
+        </guideCurveProfile>
+      </guideCurves>
+    </profiles>
+  </vehicles>
+  <toolspecific>
+    <cFD>
+      <farField>
+        <type>halfCube</type>
+        <referenceLength>10.0</referenceLength>
+        <multiplier>1.</multiplier>
+      </farField>
+    </cFD>
+  </toolspecific>
+</cpacs>
diff --git a/tests/unittests/testFuselageStandardProfileRectangle.cpp b/tests/unittests/testFuselageStandardProfileRectangle.cpp
new file mode 100644
index 000000000..3b2cd82f2
--- /dev/null
+++ b/tests/unittests/testFuselageStandardProfileRectangle.cpp
@@ -0,0 +1,175 @@
+/*
+* Copyright (C) 2022 German Aerospace Center
+* Licensed under the Apache License, Version 2.0 (the "License");
+* you may not use this file except in compliance with the License.
+* You may obtain a copy of the License at
+*
+*     http://www.apache.org/licenses/LICENSE-2.0
+*
+* Unless required by applicable law or agreed to in writing, software
+* distributed under the License is distributed on an "AS IS" BASIS,
+* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
+* See the License for the specific language governing permissions and
+* limitations under the License.
+*/
+
+#include "CTiglMakeLoft.h"
+#include "test.h"
+#include "tigl.h"
+#include "Debugging.h"
+#include "tiglcommonfunctions.h"
+#include "BRepBuilderAPI_Transform.hxx"
+#include <BRepCheck_Analyzer.hxx>
+#include "CCPACSConfigurationManager.h"
+#include "CCPACSConfiguration.h"
+#include "CNamedShape.h"
+
+class FuselageStandardProfile : public ::testing::Test
+{
+protected:
+    static void SetUpTestCase()
+    {
+        // Test case on standardProfile, mixed profiles: rectangle, rectangle with rounded corners, circle, circle with kinks
+
+        const char* filename = "TestData/simpletest_standard_profile_rectangle_circle_kink.cpacs.xml";
+        ReturnCode tixiRet;
+        TiglReturnCode tiglRet;
+
+        tiglHandle = -1;
+        tixiHandle = -1;
+
+        tixiRet = tixiOpenDocument(filename, &tixiHandle);
+        ASSERT_TRUE (tixiRet == SUCCESS);
+        tiglRet = tiglOpenCPACSConfiguration(tixiHandle, "", &tiglHandle);
+        ASSERT_TRUE(tiglRet == TIGL_SUCCESS);
+
+        // Test case on standardProfile rectangle with guide curves
+
+        const char* filename1 = "TestData/simpletest_standard_profile_rectangle_circle_guides.cpacs.xml";
+        ReturnCode tixiRet1;
+        TiglReturnCode tiglRet1;
+
+        tiglHandle1 = -1;
+        tixiHandle1 = -1;
+
+        tixiRet1 = tixiOpenDocument(filename1, &tixiHandle1);
+        ASSERT_TRUE (tixiRet1 == SUCCESS);
+        tiglRet1 = tiglOpenCPACSConfiguration(tixiHandle1, "", &tiglHandle1);
+        ASSERT_TRUE(tiglRet1 == TIGL_SUCCESS);
+
+        // Test case on standardProfile, invalid elements
+
+        ReturnCode tixiRet2;
+        TiglReturnCode tiglRet2;
+
+        tiglHandle2 = -1;
+        tixiHandle2 = -1;
+
+        tixiRet2 = tixiOpenDocument(filename1, &tixiHandle2);
+        ASSERT_TRUE (tixiRet2 == SUCCESS);
+        tiglRet2 = tiglOpenCPACSConfiguration(tixiHandle2, "", &tiglHandle2);
+        ASSERT_TRUE(tiglRet2 == TIGL_SUCCESS);
+
+    }
+
+    static void TearDownTestCase()
+    {
+        ASSERT_TRUE(tiglCloseCPACSConfiguration(tiglHandle) == TIGL_SUCCESS);
+        ASSERT_TRUE(tixiCloseDocument(tixiHandle) == SUCCESS);
+        tiglHandle = -1;
+        tixiHandle = -1;
+
+        ASSERT_TRUE(tiglCloseCPACSConfiguration(tiglHandle1) == TIGL_SUCCESS);
+        ASSERT_TRUE(tixiCloseDocument(tixiHandle1) == SUCCESS);
+        tiglHandle1 = -1;
+        tixiHandle1 = -1;
+
+        ASSERT_TRUE(tiglCloseCPACSConfiguration(tiglHandle2) == TIGL_SUCCESS);
+        ASSERT_TRUE(tixiCloseDocument(tixiHandle2) == SUCCESS);
+        tiglHandle2 = -1;
+        tixiHandle2 = -1;
+
+    }
+
+    void SetUp() override {}
+    void TearDown() override {}
+
+
+    static TixiDocumentHandle           tixiHandle;
+    static TiglCPACSConfigurationHandle tiglHandle;
+
+    static TixiDocumentHandle           tixiHandle1;
+    static TiglCPACSConfigurationHandle tiglHandle1;
+
+    static TixiDocumentHandle           tixiHandle2;
+    static TiglCPACSConfigurationHandle tiglHandle2;
+
+};
+
+TixiDocumentHandle FuselageStandardProfile::tixiHandle = 0;
+TiglCPACSConfigurationHandle FuselageStandardProfile::tiglHandle = 0;
+TixiDocumentHandle FuselageStandardProfile::tixiHandle1 = 0;
+TiglCPACSConfigurationHandle FuselageStandardProfile::tiglHandle1 = 0;
+TixiDocumentHandle FuselageStandardProfile::tixiHandle2 = 0;
+TiglCPACSConfigurationHandle FuselageStandardProfile::tiglHandle2 = 0;
+
+
+
+TEST_F(FuselageStandardProfile, BuildFuselageMixedProfilesWithKinks_ValidValues)
+{
+    // read configuration
+    tigl::CCPACSConfigurationManager& manager = tigl::CCPACSConfigurationManager::GetInstance();
+    tigl::CCPACSConfiguration& config         = manager.GetConfiguration(tiglHandle);
+    tigl::CTiglUIDManager& uidmgr = config.GetUIDManager();
+    auto fuselage = config.GetFuselage(1).GetLoft();
+    ASSERT_TRUE(BRepCheck_Analyzer(fuselage->Shape()).IsValid());
+}
+
+TEST_F(FuselageStandardProfile, BuildFuselageMixedProfilesWithGuides_ValidValues)
+{
+    // read configuration
+    tigl::CCPACSConfigurationManager& manager = tigl::CCPACSConfigurationManager::GetInstance();
+    tigl::CCPACSConfiguration& config         = manager.GetConfiguration(tiglHandle1);
+    tigl::CTiglUIDManager& uidmgr = config.GetUIDManager();
+    auto fuselage = config.GetFuselage(1).GetLoft();
+    ASSERT_TRUE(BRepCheck_Analyzer(fuselage->Shape()).IsValid());
+}
+
+TEST_F(FuselageStandardProfile, BuildFuselageMixedProfilesWithGuides_InvalidInput)
+{
+    tigl::CCPACSConfigurationManager& manager = tigl::CCPACSConfigurationManager::GetInstance();
+    //add invalid element
+    tixiCreateElementAtIndex(tixiHandle2, "/cpacs/vehicles/profiles/fuselageProfiles", "fuselageProfile", 1);
+    tixiCreateElement(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]", "invalidType");
+    tixiAddTextAttribute(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]", "uID", "std2");
+
+    // change uid of one segment to invalid profile type
+    tixiUpdateTextElement(tixiHandle2, "/cpacs/vehicles/aircraft/model/fuselages/fuselage[1]/sections/section[1]/elements/element[1]/profileUID", "std2");
+    tiglOpenCPACSConfiguration(tixiHandle2, "", &tiglHandle2);
+    tigl::CCPACSConfiguration& config1         = manager.GetConfiguration(tiglHandle2);
+
+    // fuselage cannot be build with invalid profile
+    ASSERT_THROW(config1.GetFuselage(1).GetLoft(),tigl::CTiglError);
+
+    //add  point list profile with 2 elements
+    tixiCreateElementAtIndex(tixiHandle2, "/cpacs/vehicles/profiles/fuselageProfiles", "fuselageProfile", 1);
+    tixiCreateElement(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]", "pointList");
+    tixiAddTextAttribute(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]", "uID", "pls");
+    tixiCreateElement(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]/pointList", "x");
+    tixiAddTextAttribute(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]/x", "mapType", "vector");
+    tixiAddTextElement(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]","x", "1.0;0.9");
+    tixiCreateElement(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]/pointList", "y");
+    tixiAddTextAttribute(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]/y", "mapType", "vector");
+    tixiAddTextElement(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]","y", "0.0;0.0");
+    tixiCreateElement(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]/pointList", "z");
+    tixiAddTextAttribute(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]/z", "mapType", "vector");
+    tixiAddTextElement(tixiHandle2,"/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[1]","z", "1.0;0.9");
+
+    // change uid of one segment to profile type with only two points in point list
+    tixiUpdateTextElement(tixiHandle2, "/cpacs/vehicles/aircraft/model/fuselages/fuselage[1]/sections/section[1]/elements/element[1]/profileUID", "pls");
+    tiglOpenCPACSConfiguration(tixiHandle2, "", &tiglHandle2);
+    tigl::CCPACSConfiguration& config2         = manager.GetConfiguration(tiglHandle2);
+    // fuselage cannot be build with invalid profile
+    ASSERT_THROW(config2.GetFuselage(1).GetLoft(),tigl::CTiglError);
+
+}
diff --git a/tests/unittests/testctiglbsplinealgorithms.cpp b/tests/unittests/testctiglbsplinealgorithms.cpp
index b1fd81b6e..cc8dbafaa 100644
--- a/tests/unittests/testctiglbsplinealgorithms.cpp
+++ b/tests/unittests/testctiglbsplinealgorithms.cpp
@@ -87,11 +87,28 @@ TEST(TiglBSplineAlgorithms, testComputeParamsBSplineCurve)
     ASSERT_NEAR(parameters[3], right_parameters(4), 1e-15);
 }
 
-TEST(TiglBSplineAlgorithms, testComputeParamsBSplineSurface)
+TEST(TiglBSplineAlgorithms, testCTiglPointsToBSplineInterpolation)
 {
-    // test for method computeParamsBSplineSurf
-
-    // TODO
+    // create a curve with parameters
+    std::vector<gp_Pnt> curvePnts(5);
+    curvePnts.at(0) = (gp_Pnt(0., 0., 1.));
+    curvePnts.at(1) = (gp_Pnt(0., 0.1, 1.2));
+    curvePnts.at(2) = (gp_Pnt(0., 0.2, 1.7));
+    curvePnts.at(3) = (gp_Pnt(0., 0.1, 1.5));
+    curvePnts.at(0) = (gp_Pnt(0., 0.3, 1.9));
+    std::vector<double> params = { 0.1, 0.3, 0.4, 0.5,0.9};
+    auto curve = tigl::CTiglPointsToBSplineInterpolation(curvePnts, params).Curve();
+    std::vector<gp_Pnt> curvePnts1(5);
+    curve->D0(0.1,curvePnts1[0]);
+    curve->D0(0.3,curvePnts1[1]);
+    curve->D0(0.4,curvePnts1[2]);
+    curve->D0(0.5,curvePnts1[3]);
+    curve->D0(0.9,curvePnts1[4]);
+    ASSERT_TRUE(curvePnts1[0].IsEqual(curvePnts[0], 1e-5));
+    ASSERT_TRUE(curvePnts1[1].IsEqual(curvePnts[1], 1e-5));
+    ASSERT_TRUE(curvePnts1[2].IsEqual(curvePnts[2], 1e-5));
+    ASSERT_TRUE(curvePnts1[3].IsEqual(curvePnts[3], 1e-5));
+    ASSERT_TRUE(curvePnts1[4].IsEqual(curvePnts[4], 1e-5));
 }
 
 TEST(TiglBSplineAlgorithms, testCreateCommonKnotsVectorCurve)
diff --git a/tests/unittests/tiglCommonFunctions.cpp b/tests/unittests/tiglCommonFunctions.cpp
index cd6161c63..101b55c98 100644
--- a/tests/unittests/tiglCommonFunctions.cpp
+++ b/tests/unittests/tiglCommonFunctions.cpp
@@ -15,6 +15,9 @@
 * See the License for the specific language governing permissions and
 * limitations under the License.
 */
+
+#include "CTiglMakeLoft.h"
+#include "Debugging.h"
 #include "tigl.h"
 #include "tiglcommonfunctions.h"
 #include "test.h"
@@ -28,6 +31,8 @@
 #include <BRepBuilderAPI_MakeEdge.hxx>
 #include <BRepBuilderAPI_MakeFace.hxx>
 #include <BRepBuilderAPI_MakeWire.hxx>
+#include <BRepBuilderAPI_Transform.hxx>
+#include <BRepCheck_Analyzer.hxx>
 #include <Standard_Failure.hxx>
 
 #include <list>
@@ -138,6 +143,67 @@ TEST(TiglCommonFunctions, tiglCheckPointInside_api)
 
 }
 
+TEST(TiglCommonFuctions, ApproximateArcOfCircleToRationalBSpline)
+{
+    //test valid curves
+    auto arcCurve1 = ApproximateArcOfCircleToRationalBSpline(2., 0., 5., 1.e-5, 0., 0.);
+    auto arcCurve2 = ApproximateArcOfCircleToRationalBSpline(1., 0.3, 5., 1.e-5, 0., 0.);
+    ASSERT_TRUE(GetLength(BRepBuilderAPI_MakeEdge(arcCurve1))>0.);
+    ASSERT_TRUE(!arcCurve1.IsNull());
+    ASSERT_EQ(arcCurve1->Degree(),3);
+    ASSERT_TRUE(!arcCurve2.IsNull());
+    ASSERT_EQ(arcCurve2->Degree(),3);
+    ASSERT_NO_THROW(ApproximateArcOfCircleToRationalBSpline(1., 0., 2*M_PI, 1.e-5, 0., 0.));
+    ASSERT_NO_THROW(ApproximateArcOfCircleToRationalBSpline(1., 0., M_PI/2., 1.e-5, 0., 0.));
+    //test invalid curves
+    //radius zero
+    ASSERT_THROW(ApproximateArcOfCircleToRationalBSpline(0., 0.3, 0.3, 1.e-5, 0., 0.), tigl::CTiglError);
+    //no span
+    ASSERT_THROW(ApproximateArcOfCircleToRationalBSpline(1., 0.3, 0.3, 1.e-5, 0., 0.), tigl::CTiglError);
+    ASSERT_THROW(ApproximateArcOfCircleToRationalBSpline(1., 0.0, 0.0, 1.e-5, 0., 0.), tigl::CTiglError);
+    //multiple traversion
+    ASSERT_THROW(ApproximateArcOfCircleToRationalBSpline(1., 0., 20., 1.e-5, 0., 0.), tigl::CTiglError);
+
+}
+
+TEST(TiglCommonFunctions, BuildWireRectangle_CornerRadiusZero)
+{
+    auto wire = BuildWireRectangle(1., 0.);
+    ASSERT_TRUE(wire.Closed());
+    auto trafo = gp_Trsf();
+    auto vec = gp_Vec(-1.,0.,0.);
+    trafo.SetTranslation(vec);
+    auto wire2 = BRepBuilderAPI_Transform(wire, trafo).Shape();
+    ASSERT_TRUE(wire2.Closed());
+    auto loft = CTiglMakeLoft();
+    loft.addProfiles(wire);
+    loft.addProfiles(wire2);
+    ASSERT_TRUE(BRepCheck_Analyzer(loft.Shape()).IsValid());
+
+
+}
+
+TEST(TiglCommonFunctions, BuildWireRectangle_CornerRadiusOK)
+{
+    auto wire = BuildWireRectangle(0.5, 0.14);
+    ASSERT_TRUE(wire.Closed());
+    auto trafo = gp_Trsf();
+    auto vec = gp_Vec(-1.,0.,0.);
+    trafo.SetTranslation(vec);
+    auto wire2 = BRepBuilderAPI_Transform(wire, trafo).Shape();
+    ASSERT_TRUE(wire2.Closed());
+    auto loft = CTiglMakeLoft();
+    loft.addProfiles(wire);
+    loft.addProfiles(wire2);
+    ASSERT_TRUE(BRepCheck_Analyzer(loft.Shape()).IsValid());
+}
+
+TEST(TiglCommonFunctions, BuildWireRectangle_CornerRadiusInvalid)
+{
+    ASSERT_THROW(BuildWireRectangle(0.5, 1.), tigl::CTiglError);
+    ASSERT_THROW(BuildWireRectangle(0.5, -1.), tigl::CTiglError);
+}
+
 TEST(TiglCommonFunctions, LinspaceWithBreaks)
 {
     std::vector<double> breaks;