Question: Air flows from a tank through a nozzle into the standard atmosphere, as in Fig. P9.57. A normal shock stands in the exit of the
(a) The tank pressure; and
(b) The mass flow.
14 cm2 Air at 100 10 cm I Shock ISea level air
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The throat must be sonic and the area ratio at the shock gives the Mach numb... View full answer
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