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Engineering, 01.03.2021 21:00 manou76

Consider the purely subsonic flow in a convergent-divergent duct. The inlet. throat, and exit area are 1 m', 0.7 ni', and 0.85 m', respectively. If the inlet Mach number and pressure are 0.3 and 0.8 x lo5 ~/m', respectively, calculate: a. M and p at the throat b. M and p at the exit

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Consider the purely subsonic flow in a convergent-divergent duct. The inlet. throat, and exit area a...
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