Experimental and analytical study of H sub 2-air reaction kinetics using a standing-wave normal shock.
Author:
Affiliation:
1. University of Illinois, Urbana, III.
2. ARO Inc., Arnold Air Force Station, Tenn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference29 articles.
Cited by 16 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. On the use of shock-induced combustion in hypersonic engines;Space Plane and Hypersonic Systems and Technology Conference;1996-11-18
2. Review of shock-induced supersonic combustion research and hypersonic applications;Journal of Propulsion and Power;1994-09
3. Detonation Waves and Propulsion;ICASE/LaRC Interdisciplinary Series in Science and Engineering;1994
4. A review of supersonic combustion research at AEDC with hypersonic application;29th Joint Propulsion Conference and Exhibit;1993-06-28
5. Ignition delay and characteristic reaction length in shock induced supersonic combustion;25th Joint Propulsion Conference;1989-07-12
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