Progress in hypersonic combustion technology with computation and experiment-Reference-Cited by-同舟云学术

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Progress in hypersonic combustion technology with computation and experiment

Published:1990-08-17 Issue: Volume: Page:
ISSN:
Container-title:2nd International Aerospace Planes Conference
language:
Short-container-title:

Author:

ANDERSON GRIFFIN¹,KUMAR AJAY¹,ERDOS JOHN²

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. General Applied Science Laboratories, Ronkonkoma, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-5254

Reference60 articles.

Cited by 23 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

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3. Flow Characterization of a Hypersonic Expansion Tube Facility for Supersonic Combustion Studies;Journal of Propulsion and Power;2017-11

4. Expansion Tubes in Australia;Experimental Methods of Shock Wave Research;2015-11-01

5. Production of High-Mach-Number Scramjet Flow Conditions in an Expansion Tube;AIAA Journal;2014-01

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