WorldofAerospace.googlepages.com Contact Us  Sitemap  Home  
Calculate Velocity at Throat of Supersonic Wind Tunnel


Aerospace



How to calculate the Velocity at Throat of Supersonic Wind Tunnel In order to calculate the velocity at the throat we consider a supersonic wind tunnel. 

In order to calculate, we would need,
Air temperature in the reservoir of the Wind Tunnel , T0 in Kelvin
Pressure in the reservoir of the Supersonic Wind Tunnel, P0
Static Temperature at the throat of the wind tunnel T* in Kelvin
Static Temperature at the exit of the wind tunnel Te in Kelvin
The mass flow through the nozzle in kg/sec
Cp value for air = 1008 J/kg.K
Performing the calculation and using the energy equation and the fact that V0 reservoir velocity is zero the velocity at the throat of the Supersonic Wind Tunnel is computed. 

Download Free Program to Calculate the Velocity at the throat of a Supersonic Wind Tunnel

