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Physics, 23.02.2021 01:10 bigbear123

g A large tank, at 400 kPa and 450 K, supplies air to a converging-diverging nozzle of throat area 4 cm2 and exit area 5 cm2. For what range of back pressures will the flow (a) be entirely subsonic; (b) have a shock wave inside the nozzle; (c) have oblique shocks outside the exit (i. e., over-expanded exit flow); and (d ) have supersonic expansion waves outside the exit (under-expanded exit flow)

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g A large tank, at 400 kPa and 450 K, supplies air to a converging-diverging nozzle of throat area 4...
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