YASim Wing method name clarification (SMC is not MAC).
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2 changed files with 3 additions and 3 deletions
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@ -370,7 +370,7 @@ float Airplane::compileWing(Wing* w)
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_wingsN->getNode("wing-span", true)->setFloatValue(w->getSpan());
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_wingsN->getNode("wing-span", true)->setFloatValue(w->getSpan());
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_wingsN->getNode("wing-area", true)->setFloatValue(w->getArea());
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_wingsN->getNode("wing-area", true)->setFloatValue(w->getArea());
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_wingsN->getNode("aspect-ratio", true)->setFloatValue(w->getAspectRatio());
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_wingsN->getNode("aspect-ratio", true)->setFloatValue(w->getAspectRatio());
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_wingsN->getNode("mean-chord", true)->setFloatValue(w->getMAC());
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_wingsN->getNode("standard-mean-chord", true)->setFloatValue(w->getSMC());
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}
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}
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float wgt = 0;
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float wgt = 0;
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@ -73,7 +73,7 @@ public:
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float getSpan() { return _wingspan; };
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float getSpan() { return _wingspan; };
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float getArea() { return _wingspan*_meanChord; };
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float getArea() { return _wingspan*_meanChord; };
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float getAspectRatio() { return _aspectRatio; };
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float getAspectRatio() { return _aspectRatio; };
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float getMAC() { return _meanChord; };
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float getSMC() { return _meanChord; };
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int numSurfaces() { return _surfs.size(); }
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int numSurfaces() { return _surfs.size(); }
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Surface* getSurface(int n) { return ((SurfRec*)_surfs.get(n))->surface; }
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Surface* getSurface(int n) { return ((SurfRec*)_surfs.get(n))->surface; }
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@ -113,7 +113,7 @@ private:
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// calculated from above
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// calculated from above
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float _tip[3];
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float _tip[3];
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float _meanChord;
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float _meanChord; // std. mean chord
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float _wingspan;
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float _wingspan;
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float _aspectRatio;
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float _aspectRatio;
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