Three-Dimensional Simulations of Bleed-Hole Rows/ Shock-Wave/Turbulent Boundary-Layer Interactions-Reference-Cited by-同舟云学术

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Three-Dimensional Simulations of Bleed-Hole Rows/ Shock-Wave/Turbulent Boundary-Layer Interactions

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

Hamed Awatef¹,Morell Albert¹,Manavasi Seshagopal¹

Affiliation:

1. University of Cincinnati

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-840

Reference42 articles.

1. Investigation of the Stall Hammershock at the Engine Inlet

2. Conservation Coupling Technique for Dynamic Inlet-Engine Analyses

3. Prediction of supersonic inlet unstart caused by freestream disturbances

Cited by 5 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. Effects of Number of Bleed Holes on Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator;Journal of Thermal Science;2024-01-10

2. Simultaneous pressure and displacement measurements on a 3D flexible surface in a supersonic flow;AIAA Scitech 2020 Forum;2020-01-05

3. Recent Advances in Propulsion Research at the University of Cincinnati;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

4. Aerothermal characteristics of bleed slot in hypersonic flows;Science China Physics, Mechanics & Astronomy;2015-09-05

5. Theoretical analysis of effects of boundary layer bleed on scramjet thrust;Science China Physics, Mechanics and Astronomy;2013-09-21

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