Large-flow reverse jet flow test device and method for hypersonic aircraft
A test device, hypersonic technology, applied in the field of large flow reverse jet flow test device, to achieve the effect of improving test efficiency, high measurement accuracy and avoiding adverse effects
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[0069] The large-flow reverse jet flow test device for hypersonic aircraft in this embodiment has four test nozzles 6 and one debugging nozzle 9, and the debugging nozzle 9 can replace any one of the testing nozzles 6.
[0070] The high-flow reverse jet flow test method for hypersonic aircraft in this embodiment uses high-pressure air as the jet flow medium, the wind tunnel wall air source adapter is externally connected to the high-pressure air source, the wind tunnel wall air source adapter, and the middle bracket The upper Φ15mm interface and the air inlet 2 are connected by a Φ19×2mm copper tube, and the high-pressure air enters the airflow channel from the air inlet 2, and is ejected from the corresponding test nozzle 6 through the branch pipes. The ventilation area of the anti-jet engine chamber formed by each branch pipe is 78.5mm 2 , the Laval nozzle throat area of test nozzle 6 is 15.9mm 2 , the flow velocity of high-pressure air in the branch pipeline is about 4...
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