.: code Clift(N)

Calculates main flight parameters based on International Standard Atmosphere (ISA) model.
The user interface is implemented using FOX toolkit library.
Use "." as decimal separator on Windows platforms.

.: initial data:

Mach Mach number
H Altitude
n Overload
G Weight (ton)
Lref Reference lenght
Sref Reference wing area

.: computation results:

C lift lift coefficient
Re number Reynolds number
U speed
a speed of sound
T ref temperature
Mu dynamic viscosity
Nu kinematic viscosity
Rho density
P pressure
0.5*Rho*U*U dynamic head
S*0.5*Rho*U*U wing loading