Control on SWBLI by vortex generator in a supersonic cascade-Reference-Cited by-同舟云学术

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Control on SWBLI by vortex generator in a supersonic cascade

Published:2024-08 Issue: Volume:151 Page:109323
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Zhongyi,Song Tianchu,Chen Xiaohu,Wang Meng

Funder

National High-tech Research and Development Program

Fundamental Research Funds for the Central Universities

National Major Science and Technology Projects of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference38 articles.

1. Compressor Aerodynamics. M;Cumpsty,1989

2. Fifty years of shock wave/boundary layer interaction——What next?[J];Dolling;AIAA J.,2000

3. Effect of vortex generators on transonic swept wings[J];Ito;J. Aircr.,2016

4. Pressure wave damping in transonic airfoil flow by means of micro vortex generators[J];Gageik;Aerosp. Sci. Technol.,2016

5. Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows[J];Huang;Acta Astronaut.,2020

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