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Published in 2018 at "AIAA Journal"
DOI: 10.2514/1.j056460
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...
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Keywords:
shock;
vane type;
control incident;
incident shock ... See more keywords