Boundary-layer instability on sharp cone at Mach 3.5 with controlled input-Reference-Cited by-同舟云学术

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Boundary-layer instability on sharp cone at Mach 3.5 with controlled input

Published:2002-01 Issue: Volume:40 Page:1015-1018
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Corke T. C.,Cavalieri D. A.,Matlis E.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 8 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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2. Experimental Investigation of the Structure of Disturbances from Two Pulsed Sources in the Flat-Plate Supersonic Boundary Layer;Известия Российской академии наук. Механика жидкости и газа;2023-07-01

3. Effects of plasma kinetic modeling on performance characterization of plasma actuators for active flow control;E3S Web of Conferences;2020

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