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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j059006
Abstract: Extensive wind-tunnel tests were performed on a Y-shaped diverterless supersonic inlet (DSI). All tests were conducted at a free stream Mach number of M∞=1.65, the design Mach number for this inlet...
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Keywords:
inlet;
flow asymmetry;
shaped diverterless;
diverterless supersonic ... See more keywords