Studies on Leading Edge Detection in Mechanically- and Combustion-Generated Shock Trains in Dual-Mode Scramjet Engines-Reference-Cited by-同舟云学术

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Studies on Leading Edge Detection in Mechanically- and Combustion-Generated Shock Trains in Dual-Mode Scramjet Engines

Published:2017-01-05 Issue: Volume: Page:
ISSN:
Container-title:55th AIAA Aerospace Sciences Meeting
language:
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Author:

Ladeinde Foluso¹,Lou Zhipeng²,Kim D.-H.³,Das Rajarshi³

Affiliation:

1. SUNY Korea

2. Stony Brook University

3. Andong National University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0556

Reference31 articles.

1. Shock train and pseudo-shock phenomena in internal gas flows

2. Jones, T.P. & Baumann, E. 2003. Evaluation of the X-43A Scramjet Engine Controller Performance by Monte Carlo Technique. NASA/TM-2003-212036.

3. Unstart Margin Characterization Method of Scramjet Considering Isolator–Combustor Interactions

Cited by 4 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. Pressure Effects in a Scramjet Combustor;AIAA Propulsion and Energy 2021 Forum;2021-07-28

2. The Effects of Isolator Length on Combustion in a Scramjet Engine Model;AIAA Propulsion and Energy 2020 Forum;2020-08-17

3. Distinguishing Characteristics of Thermally- and Mechanically-Generated Backpressure;AIAA Scitech 2019 Forum;2019-01-06

4. On the Backpressure Phenomenon in Modeled Dual-Mode Scramjets;2018 Joint Propulsion Conference;2018-07-08

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