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a subsonic airplane is flying at a 3000-m altitude where the atmospheric conditions are 70109 kpa and 26865 k a pitot
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air enters a converging-diverging nozzle of a supersonic wind tunnel at 150 psia and 100degf with a low velocity the
air at 900 kpa and 400 k enters a converging nozzle with a negligible velocity the throat area of the nozzle is 10 cm2
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in air-conditioning applications the temperature of air is measured by inserting a probe into the flow stream thus the
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air at 300 k is flowing in a duct at a velocity of a 1 b 10 c 100 and d 1000 ms determine the temperature that a
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