Fix/lifting line without fuselage

Fixed lifting line interface to run for BWB

Description

Had to remove fuselage entries, so that BWB can becalculated

This MR is needed to run MR !269

liftingLineInterface2/include/liftingLineInterface2/liftingLineInput.h

@@ -82,7 +82,7 @@ class LIFTINGLINEINTERFACEDLLEXPORT liftingLineInput {
      *  \param aCoG {x,y,z}-coordinates of the center of gravity of the aircraft, [m]
      */
     void createLiftingLineInput(const std::vector<geom2::MultisectionSurface<geom2::AirfoilSection>>& liftingSurfaces,
-                                const geom2::MultisectionSurface<geom2::PolygonSection>& theFuselage,
+                                const std::vector<double>& fuselageWidths,
                                 const double& aMachNumber, const double& aReynoldsnumber, const double& refArea, const Point& aCoG);
     /** \brief Method to initialize liftingLine run.
      *  \details Method differentiates between compressible and incompressible.