Experimental investigation of incident shock wave/boundary layer interaction controlled by pulsed spark discharge array-Reference-Cited by-同舟云学术

Experimental investigation of incident shock wave/boundary layer interaction controlled by pulsed spark discharge array

Published:2022-04 Issue: Volume:132 Page:110515
ISSN:0894-1777
Container-title:Experimental Thermal and Fluid Science
language:en
Short-container-title:Experimental Thermal and Fluid Science

Author:

Yanhao Luo,Hua Liang,Jun Li,Shanguang Guo,Mengxiao Tang,Weiliang Kong

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference30 articles.

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3. Y. Yao, B. Gao. Flow structure of incident shock wave boundary layer interaction with separation. Acta Aerodynamica Sinica. 37(2019) 740-747 [Chinese].

4. Dolling, S. David. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next. AIAA Journal. 39(2001) 1517-1531.

5. Experimental Results with Airfoils Tested in the High-speed Tunnel at Guidonia;Ferri;Natl Advisory Committee for Aeronautics.,1940

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