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Calculate Area Ratio for Supersonic Wind Tunnel Method to Calculate the Temperature Area Ratio for Supersonic Wind Tunnel 

Aerospace



How to Calculate the Area Ratio for a Supersonic Wind Tunnel 

In order to calculate the Area Ratio for a supersonic wind tunnel we consider the standard sealevel conditions with SI units.
For this purpose, we require the flow through the Mach Tunnel.
Performing the calculation, gives us the value of the Area Ratio for Supersonic Wind Tunnel Ae/At where, Ae is the Area of the Exit and At is the Area of the Throat. 

Download Free Program to Calculate the Area Ratio for a Supersonic Wind Tunnel

