From 21e69b056888bea62fff1e0ce2da69fb6ed90ad9 Mon Sep 17 00:00:00 2001
From: Maurice Zimmnau <zimmnau@ilr.rwth-aachen.de>
Date: Thu, 20 Feb 2025 14:38:33 +0100
Subject: [PATCH] Apply 1 suggestion(s) to 1 file(s)
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Co-authored-by: Florian Schültke <florian.schueltke@ilr.rwth-aachen.de>
---
aerodynamic_analysis/src/methods/liftingLineForTAW.cpp | 2 +-
1 file changed, 1 insertion(+), 1 deletion(-)
diff --git a/aerodynamic_analysis/src/methods/liftingLineForTAW.cpp b/aerodynamic_analysis/src/methods/liftingLineForTAW.cpp
index 834def0d..529559c2 100644
--- a/aerodynamic_analysis/src/methods/liftingLineForTAW.cpp
+++ b/aerodynamic_analysis/src/methods/liftingLineForTAW.cpp
@@ -825,7 +825,7 @@ double liftingLineForTAW::getFuselageCM_AeroCenterCorrection(const uint16_t& mac
* (myAcftPt->theFuselage.at(0).maxWidth * myAcftPt->theFuselage.at(0).maxHeight * l_fn)
/ (myAcftPt->Sref * myAcftPt->theWing.at(0).l_mu_right);
*/
- double delta_fus_1 = - 1.8 / (convertRadian(DEGREE, myLL_vec.at(machID).theLLOutputPt->dCLtodAoA_wf))
+ double delta_fus_1 = - 1.8 / (convertUnit(RADIAN, DEGREE, myLL_vec.at(machID).theLLOutputPt->dCLtodAoA_wf))
* (geom2::measure::width_max(theFuselage) * geom2::measure::height_max(theFuselage) * l_fn)
/ (geom2::measure::reference_area(liftingSurfaces.front()) * geom2::measure::mean_aerodynamic_chord(liftingSurfaces.front()));
// [Tor13] (E-38): delta_f2 -> accounts for lift loss in the region where wing/fuselage lift carry-over is concentrated
--
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