Engineering, 06.03.2020 15:57 kaliyab191
In the flow past a compression corner, the upstream Mach number and static pressure are 3.5 and 1 atm, respectively. Downstream of the corner, the pressure is 5.48 atm. Calculate the deflection angle of the corner.
Answers: 2
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In the flow past a compression corner, the upstream Mach number and static pressure are 3.5 and 1 at...
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