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An experimental investigation was conducted to control an incident shock-induced boundary-layer separation associated with a 14 deg shock generator in a Mach 2.05 flow. Two vane-type configurations... Click to show full abstract
An experimental investigation was conducted to control an incident shock-induced boundary-layer separation associated with a 14 deg shock generator in a Mach 2.05 flow. Two vane-type configurations...
Keywords:
shock;
vane type;
control incident;
incident shock;
shock induced
Journal Title: AIAA Journal
Year Published: 2018
Link to full text (if available)
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Journal Title: AIAA Journal
Year Published: 2018
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!