Research on Supersonic Inlet Bleed-Reference-Cited by-同舟云学术

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Research on Supersonic Inlet Bleed

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:

Davis David¹,Vyas Manan¹,Slater John¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-272

Reference11 articles.

1. Improvements in Modeling 90-degree Bleed Holes for Supersonic Inlets

2. Flow coefficient behavior for boundary layer bleed holes and slots

3. Experimental investigation of the effect of a single bleed hole on a supersonic turbulent boundary-layer

Cited by 15 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 bleed pressure on shock-wave/boundary-layer interactions in a transonic compressor stator with suction holes;International Journal of Turbo & Jet-Engines;2024-04-16

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

3. Effects of bleed hole size on supersonic boundary layer bleed mass flow rate;Journal of Zhejiang University-SCIENCE A;2020-08

4. Supersonic Bleed Rate Model for a Circular Orifice Based on Geometric Similarity;AIAA Journal;2020-06

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

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