Fix stall widths for the "auxilliary" (reverse flow) stalls so they

are sharp, as intended.  These were are never seen in practice; I
found the problem while looking at 360 degree lift curve graphs
looking for discontinuities.

diff --git a/src/FDM/YASim/Wing.cpp b/src/FDM/YASim/Wing.cpp
index 8816cfa994617f83e1c2ac5da556c6cedb19524b..5c9fd6a33a6b1542fea0fe874b1a3bc6fbdf8d08 100644 (file)
--- a/src/FDM/YASim/Wing.cpp
+++ b/src/FDM/YASim/Wing.cpp
@@ -433,7 +433,7 @@ Surface* Wing::newSurface(float* pos, float* orient, float chord,
     int i;
     for(i=2; i<4; i++) {
         s->setStall(i, 0.2267f);
-        s->setStallWidth(i, 1);
+        s->setStallWidth(i, 0.01);
     }
     
     if(flap0)   s->setFlapParams(_flap0Lift, _flap0Drag);