Fixed stupid output error on steady forces calc
@@ -92,11 +92,11 @@ class AeroForcesSteadyCalculator(BaseSolver):
total_force += np.dot(rot.T, force[i_surf][0:3, i_m, i_n])
lift = total_force[2]
- cout.cout_wrap('Lift = %f6 (N)' % lift)
+ cout.cout_wrap('Lift = %f (N)' % lift)
drag = total_force[0]
- cout.cout_wrap('Drag= %f6 (N)' % drag)
+ cout.cout_wrap('Drag= %f (N)' % drag)
side_force = total_force[1]
- cout.cout_wrap('Side force = %f6 (N)' % side_force)
+ cout.cout_wrap('Side force = %f (N)' % side_force)
# CL
# cl = total_force[2]/dynamic_pressure
