Suppression of strong shock boundary layer interaction in supersonicinlets by boundary layer blowing-Reference-Cited by-同舟云学术

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Suppression of strong shock boundary layer interaction in supersonicinlets by boundary layer blowing

Published:1975-08-16 Issue: Volume: Page:
ISSN:
Container-title:11th Propulsion Conference
language:
Short-container-title:

Author:

WONG W.¹,HALL G.¹

Affiliation:

1. Northrop Corp., Aircraft Div., Hawthorne, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1975-1209

Cited by 6 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

1. Off- and on-surface studies on flow development from various vortex generators configurations at Mach 2.0;Physics of Fluids;2021-09

2. Control of Compression-Ramp-Induced Interaction with Steady Microjets;AIAA Journal;2019-07

3. Control of Shock-Induced Boundary Layer Separation by High Momentum Blowing;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

4. An Investigation of Active Flowfield Control for Inlet Shock/Boundary Layer Interaction;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

5. Upstream Blowing Jet on Transonic Convex-Corner Flow;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

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