static const double AOA[HUIT] = {-180*RAD,-135*RAD,-90*RAD,-45*RAD,45*RAD,90*RAD,135*RAD,180*RAD
static const double CL[HUIT] = { 0, +0.3, 0, -0.3, +0.3, 0, -0.3, 0};//LIFT COEF
I have some trouble to enderstand CL ?
CL = L/(Q*A)
L= LIFT FORCE IN NEWTON
Q= DYNAMIC PRESSURE = (.5*P*(V^2))...