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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... Click to show full 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...
Keywords:
deformable shape;
cowl shock;
shock boundary;
boundary layer;
shape memory;
memory alloy
Journal Title: AIAA Journal
Year Published: 2019
Link to full text (if available)
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Journal Title: AIAA Journal
Year Published: 2019
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!