Computational fluid dynamics analysis of cavity flame holders for scramjets-Reference-Cited by-同舟云学术

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Computational fluid dynamics analysis of cavity flame holders for scramjets

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Davis D.¹,Bowersox R.²,Davis D.¹,Bowersox R.²

Affiliation:

1. USAF, Wright Lab., Wright-Patterson AFB, OH

2. USAF, Inst. of Technology, Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3270

Reference34 articles.

1. Mixing and Combustion Issues in Hypersonic Air-Breathing Propulsion

2. Davis, D.L.andBowersox, R.D.W."Stirred Reactor Analysis of Cavity Flame Holders for Scramjets," AIAA-97-3274.

Cited by 17 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. Blowoff and bulk mode instability in a liquid-fueled ramjet combustor;AIAA SCITECH 2023 Forum;2023-01-19

2. Numerical investigation on the extrusive and intrusive subcavity types and their location on the primary recirculation zone for the supersonic turbulent flow through cavity type flameholders;Thermal Science and Engineering Progress;2021-10

3. Experimental Investigation of a Solid Fuel Scramjet Using an Arc Heater;Journal of Propulsion and Power;2019-07

4. Optimization of scramjet performance with different fuel injection techniques and flame holder cavities;Acta Astronautica;2018-11

5. Ignition Experiments of Hydrocarbons in a Mach 8 Shape-Transitioning Scramjet Engine;Journal of Propulsion and Power;2016-11

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