InfamusLove5031 InfamusLove5031

08-03-2024
Physics

contestada

The Mach number, Temperature, and Pressure of air upstream of a normal shock are 2.9, 290 K, and 1.94 atm, respectively. What is the TOTAL PRESSURE downstream of the shock?
a) 2.20 atm
b) 1.75 atm
c) 2.41 atm
d) 1.29 atm

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