Control of Cowl-Shock/Boundary-Layer Interactions by Deformable Shape-Memory Alloy Bump
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DOI: 10.2514/1.j057409
Abstract: A deformable shape-memory alloy (SMA) bump is introduced to control the succeeding cowl-shock/boundary-layer interactions in a supersonic inlet with an operating Mach range of 2.0–3.8. The deformat... read more here.
Keywords: deformable shape; cowl shock; shock boundary; boundary layer ... See more keywords