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The report investigates the effects of bleed on shock wave-boundary layer interactions in a mixed-compression supersonic inlet designed for Mach 2.50. It concludes that optimal bleed occurs when approximately half of the boundary layer mass flow is bled off, with upstream or downstream bleeding being preferable to across-shock bleeding. The study also notes that slanted bleed holes perform better than normal holes in reducing boundary layer thickness.

Author

humanamiri85

Language

EN