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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… Click to show full 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...
Keywords:
inlet;
flow asymmetry;
shaped diverterless;
diverterless supersonic;
supersonic inlet
Journal Title: AIAA Journal
Year Published: 2020
Link to full text (if available)
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Journal Title: AIAA Journal
Year Published: 2020
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!