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Calculate Reservoir Pressure and Reservoir Temperature for Supersonic Wind Tunnel Method to Calculate Reservoir Pressure and Reservoir Temperature for a Supersonic Wind Tunnel 

Aerospace



How to Calculate the Reservoir Pressure and the Reservoir Temperature for the Supersonic Wind Tunnel 

In order to calculate the Reservoir Pressure and the Reservoir Temperature 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 reservoir Pressure, P0 in the units N/m^2. The reservoir Temperature T0 for Supersonic Wind tunnel is computed in the units of Kelvin.


Download Free Program to Calculate the Reservoir Pressure for a Supersonic Wind Tunnel

