Numerical study on the periodic control of supersonic compression corner flow using a nanosecond pulsed plasma actuator

Author:

Chen ZongnanORCID,Hao Jiaao,Wen Chih-Yung

Funder

National Natural Science Foundation of China

Research Grants Council, University Grants Committee

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference56 articles.

1. Response of hypersonic compression corner flow to upstream disturbances;Hao;J. Fluid Mech.,2023

2. Occurrence of global instability in hypersonic compression corner flow;Hao;J. Fluid Mech.,2021

3. On the origins of unsteadiness and three-dimensionality in a laminar separation bubble;Theofilis;Philos. Trans. R. Soc. London Ser. A Math. Phys. Eng. Sci.,2000

4. Global linear instability;Theofilis;Annu. Rev. Fluid Mech.,2011

5. Bifurcations in shock-wave/laminar-boundary-layer interaction: global instability approach;Robinet;J. Fluid Mech.,2007

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