Mechanism of Mixing Enhanced by Pseudo-Shock Wave-Reference-Cited by-同舟云学术

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Mechanism of Mixing Enhanced by Pseudo-Shock Wave

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Yamauchi Hideki¹,Choi Byongil¹,Kouchi Toshinori¹,Masuya Goro¹

Affiliation:

1. Tohoku University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-25

Reference17 articles.

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

2. Research on supersonic combustion

3. Demonstration of mode transition in a scramjet combustor

4. Comparison of Scramjet Engine Performance in Mach 6 Vitiated and Storage-Heated Air

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. Influences of wall vibration on shock train structures and performance of two-dimensional rectangular isolators in scramjet engine;Acta Astronautica;2020-01

2. Numerical investigation on three-dimensional shock train structures in rectangular isolators;European Journal of Mechanics - B/Fluids;2018-11

3. Effect of shock interactions on mixing layer between co-flowing supersonic flows in a confined duct;Shock Waves;2017-04-12

4. Indraft Supersonic Wind Tunnel for Shock Train Investigations;30th International Symposium on Shock Waves 2;2017

5. Pseudo-shock waves and their interactions in high-speed intakes;Progress in Aerospace Sciences;2016-04

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