Engineering, 31.03.2020 03:00 skyhe34
Consider the subsonic flow through a divergent duct with area ratio of A2/A1 = 1.7. If the inlet conditions are T1 = 300 K and u1 = 250 m/s, and the pressure at the exit is P2 = 1 atm, calculate: a. Inlet pressure P1 and b. Exit velocity u2.
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Consider the subsonic flow through a divergent duct with area ratio of A2/A1 = 1.7. If the inlet con...
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