Program: Aircraft Stall Speed
By: Jan Zumwalt - ZoomAviation.com
Update: The latest version can be found at ZoomAviation.com
Coefficient of Lift (cl)
Wing area (sqft)
Solved: Stall speed
Note: The calculated stall speed of this program is
usually within 1-2%. Of course the most critical
factor is wing CL.
Coefficient of Lift (cl): Values for common aircraft
C172, C150..... 1.5 2.20
B747 ......... 0.9 1.76
NACA0012 ...... 1.2
Clark Y ...... 1.6
Made C150 data default.
Created initial ver 1.0 and tested.
No apparent problems with code.