Mach 3.5 Compression Corner Control Using Microvortex Generators
An experimental investigation has been performed to examine the effect of vortex generators (VGs) on a compression corner flow separation. Experiments are conducted at Mach 3.5 along a 23° compression corner with turbulent inflow boundary-layer and Reynolds number [Formula: see text] based on the 6....
| Main Authors: | , , , |
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| Format: | Article |
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American Institute of Aeronautics and Astronautics (AIAA)
2024
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| Online Access: | https://hdl.handle.net/1721.1/153917 |