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Co-authored-by: Florian Schültke <florian.schueltke@ilr.rwth-aachen.de>

aerodynamic_analysis/src/methods/liftingLineForTAW.cpp

@@ -811,7 +811,7 @@ double liftingLineForTAW::getFuselageCM0(const uint16_t& machID) {
     double deltaFuselage = -1.8 * (1. - 2.5 * geom2::measure::width_max(theFuselage) / geom2::measure::length(theFuselage))
                            * (PI * geom2::measure::width_max(theFuselage) * geom2::measure::height_max(theFuselage) * geom2::measure::length(theFuselage))
                            / (4. * geom2::measure::reference_area(liftingSurfaces.front()) * geom2::measure::mean_aerodynamic_chord(liftingSurfaces.front()))
-                           * (myLL_vec.at(machID).theLLOutputPt->CLatAoA0 / ( convertRadian(DEGREE, myLL_vec.at(machID).theLLOutputPt->dCLtodAoA_wf)));
+                           * (myLL_vec.at(machID).theLLOutputPt->CLatAoA0 / ( convertUnit(RADIAN, DEGREE, myLL_vec.at(machID).theLLOutputPt->dCLtodAoA_wf)));
     return deltaFuselage;
 }