YASIM: method name clarification (and indention)

src/FDM/YASim/Airplane.cpp

@@ -787,13 +787,13 @@ void Airplane::applyDragFactor(float factor)
     float applied = Math::pow(factor, SOLVE_TWEAK);
     _dragFactor *= applied;
     if(_wing)
-      _wing->setDragScale(_wing->getDragScale() * applied);
+      _wing->multiplyDragCoefficient(applied);
     if(_tail)
-      _tail->setDragScale(_tail->getDragScale() * applied);
+      _tail->multiplyDragCoefficient(applied);
     int i;
     for(i=0; i<_vstabs.size(); i++) {
         Wing* w = (Wing*)_vstabs.get(i);
-	w->setDragScale(w->getDragScale() * applied);
+        w->multiplyDragCoefficient(applied);
     }
     for(i=0; i<_fuselages.size(); i++) {
         Fuselage* f = (Fuselage*)_fuselages.get(i);

src/FDM/YASim/FGFDM.cpp

@@ -853,7 +853,7 @@ Wing* FGFDM::parseWing(XMLAttributes* a, const char* type, Version * version)
     w->setInducedDrag(0.7*attrf(a, "idrag", 1));
 
     float effect = attrf(a, "effectiveness", 1);
-    w->setDragScale(w->getDragScale()*effect);
+    w->multiplyDragCoefficient(effect);
 
     _currObj = w;
     return w;

src/FDM/YASim/Wing.cpp

@@ -253,7 +253,7 @@ void Wing::addSurface(Surface* s, float weight, float twist)
     _surfs.add(sr);
 }
 
-void Wing::setDragScale(float scale)
+void Wing::setDragCoefficient(float scale)
 {
     _dragScale = scale;
     for(int i=0; i<_surfs.size(); i++) {
@@ -262,6 +262,11 @@ void Wing::setDragScale(float scale)
     }
 }
 
+void Wing::multiplyDragCoefficient(float factor)
+{
+    setDragCoefficient(_dragScale * factor);
+}
+
 void Wing::setLiftRatio(float ratio)
 {
     _liftRatio = ratio;

src/FDM/YASim/Wing.hpp

@@ -90,8 +90,8 @@ public:
 
     // The overall drag coefficient for the wing as a whole.  Units are
     // arbitrary.
-    void setDragScale(float scale);
+    void setDragCoefficient(float scale);
-    float getDragScale() const { return _dragScale; }
+    void multiplyDragCoefficient(float factor);
 
     // The ratio of force along the Z (lift) direction of each wing
     // segment to that along the X (drag) direction.