Engineering, 31.03.2020 00:35, lflugo6oyn4sp

The reservoir pressure of a supersonic wind tunnel is 5 atm. A static pressure probe is moved along the centerline of the nozzle, taking measurements at various stations. For these probe measurements, calculate the local Mach number and area ratio: a. 4 atm; b. 2.64 atm; c. 0.5 atm.

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The reservoir pressure of a supersonic wind tunnel is 5 atm. A static pressure probe is moved along...