The reservoir pressure and temperature for a blowdown

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Reference no: EM13630794

The reservoir pressure and temperature for a blowdown supersonic wind tunnel are 7.5 atm and 800 deg R, respectively. The design Mach number for the tunnel is Mdes = 3.5. Compute the exit Mach number and exit velocity (in ft/s) for the back pressure pb=7.48atm

Reference no: EM13630794

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