Comparison of Bleed and Micro-Vortex Generator Effects on Supersonic Boundary-Layers-Reference-Cited by-同舟云学术

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Comparison of Bleed and Micro-Vortex Generator Effects on Supersonic Boundary-Layers

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Oorebeek Joseph¹,Nolan William¹,Babinsky Holger¹

Affiliation:

1. University of Cambridge

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-45

Reference27 articles.

1. 1Syberg, J. and Hickcox, T. E. “Design of a Bleed System for a Mach 3.5 Inlet,” Tech. Rep. January, 1973.

2. Control of shock-wave boundary-layer interactions by bleed in supersonic mixed compression inlets

3. Survey of validation data base for shockwave boundary-layer interactions in supersonic inlets

4. Flowfield measurements in a normal-hole-bled oblique shock-wave and turbulent boundary-layer interaction

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. Parameter Influence on the Porous Bleed Performance with & without Shock-Boundary Layer Interaction;AIAA AVIATION 2022 Forum;2022-06-20

2. External-Compression Supersonic Inlet Free from Violent Buzz;AIAA Journal;2019-06

3. CFD Investigation Using Bleed as a Method of Active Flow Control;55th AIAA Aerospace Sciences Meeting;2017-01-05

4. Progress in shock wave/boundary layer interactions;Progress in Aerospace Sciences;2015-01

5. Progress in Shock Wave/Boundary Layer Interactions;43rd Fluid Dynamics Conference;2013-06-22

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