Study of Unsteady, Sphere-Driven, Shock-Induced Combustion for Application to Hypervelocity Airbreathing Propulsion-Reference-Cited by-同舟云学术

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Study of Unsteady, Sphere-Driven, Shock-Induced Combustion for Application to Hypervelocity Airbreathing Propulsion

Published:2011-07-31 Issue: Volume: Page:
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Container-title:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Axdahl Erik,Kumar Ajay,Wilhite Alan

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. [1]Menees, G. P., Adelman, H. G., Bowles, J. V., and Cambier, J.L., Wave combustors for trans-atmospheric vehicles, Journal of Propulsion andPower, Vol.8, No. 3,May1992, pp. 709-713.

2. Unsteady Shock-Induced Combustion Past Blunt Bodies

3. Mechanism of Instabilities of Exothermic Hypersonic Blunt-Body Flows

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. An improved uncoupled finite volume solver for simulating unsteady shock-induced combustion;Computers & Fluids;2018-05

2. Numerical Investigation of the Effects of Nonuniform Premixing on Shock-Induced Combustion;AIAA Journal;2016-05

3. Mitigation of Autoignition Due to Premixing in a Hypervelocity Flow Using Active Wall Cooling;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12

4. Study of Forebody Injection and Mixing with Application to Hypervelocity Airbreathing Propulsion;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30

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