Swept shock wave/boundary layer interaction control based on surface arc plasma
Author:
Affiliation:
1. Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an 710038, People's Republic of China
2. School of Mechanical Engineering, Xi'an Jiaotong University, Xi'an 710048, People's Republic of China
Abstract
Funder
National Science and Technology Major Project
National Outstanding Youth Foundation of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0100630
Reference63 articles.
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3. Upstream-Influence Scaling of Fin-Induced Laminar Shockwave/Boundary-Layer Interactions
4. Quasi-Conical Free Interaction in Fin-Induced Shock Wave/Laminar Boundary-Layer Interactions
5. J. Délery , J. G. Marvin , and E. Reshotko , “ Shock-wave boundary layer interactions,” Report No. AGARD-AG-280, Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine (France), 1986.
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