Wing Optimizer

Made using the calculation code from NASA's FoilSim

Input values

Airspeed (mph):

Altitude (feet):

Wing area (square feet):

Optimization function (to be maximized):





Wing profile nomenclature

Output parameters

Optimal angle of attack (degrees):

Optimal camber (percent):

Optimal thickness (percent):

Lift and drag with optimal parameters

Resulting lift (lbf):

Resulting drag (lbf):

Resulting LDR: