Instabilities and transition in the wall boundary layers of low-disturbance supersonic nozzles

Author:

CHEN F.-J.1,MALIK M.1,BECKWITH I.1

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Reference48 articles.

Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

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3. Görtler instability analysis of Mach 6 flow on a flared axisymmetric cone with and without suction;AIAA Aviation 2019 Forum;2019-06-14

4. Development of Hypersonic Quiet Tunnels;Journal of Spacecraft and Rockets;2008-07

5. An Experimental Study of Görtler Vortices in Compressible Flow;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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