.: initial data:
Mach | Mach number |
H | Altitude |
n | Overload |
G | Weight (ton) |
Lref | Reference lenght |
Sref | Reference wing area |
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.: 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 |
|