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Yun Wu

affiliation not provided to SSRN

SCHOLARLY PAPERS

1

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32

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0

Scholarly Papers (1)

1.

Supersonic Cavity Flow Control at Different Geometrical Configuration Using Plasma Actuator Array

Number of pages: 22 Posted: 27 May 2025
Air Force Engineering University, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and Air Force Engineering University
Downloads 32 (1,332,057)

Abstract:

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supersonic cavity flow, flow control, plasma actuator array, geometrical parameter, cavity shear layer