Numerical Investigation of Bleed Effects on Supersonic Inlet under Various Bleed and Inlet Conditions-Reference-Cited by-同舟云学术

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Numerical Investigation of Bleed Effects on Supersonic Inlet under Various Bleed and Inlet Conditions

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA Applied Aerodynamics Conference
language:
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Author:

Choe Yohan¹,Kim Chongam¹

Affiliation:

1. Seoul National University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3564

Reference24 articles.

1. Bleed System Design Technology for Supersonic Inlets

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

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

4. Boundary layer development downstream of a bleed mass flow removal region

Cited by 3 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. Mixed Compression Air-Intake Design for High-Speed Transportation;Springer Proceedings in Mathematics & Statistics;2021

2. Supersonic Inlet Design using Bleed Boundary Condition with Porosity Variation and Expansion Wave;2018 AIAA Aerospace Sciences Meeting;2018-01-07

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

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