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During high-incidence maneuvers, shock-wave/boundary-layer interactions can develop over transonic inlet lower lips, significantly impacting aerodynamic performance. Here, a novel experimental rig ... Click to show full abstract
During high-incidence maneuvers, shock-wave/boundary-layer interactions can develop over transonic inlet lower lips, significantly impacting aerodynamic performance. Here, a novel experimental rig ...
Keywords:
boundary layer;
normal shock;
high incidence;
layer interactions
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!