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Control over the fluid flow becomes essential when one strives for the efficiency in aerospace vehicles and subsystems. Micro ramps are potentially optimal devices to achieve such control. The present study shows how changing their geometry changes the flow field in the supersonic turbulent boundary layer. With experimental calibration, the present study also allows predicting the influence of geometry on the micro ramp wake.

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This page is a summary of: Relation Between Geometry and Wake Characteristics of a Supersonic Microramp, AIAA Journal, April 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059868.
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