Combustion Efficiencies of Supersonic Flames
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109-2118
2. Chungnam National University, Taejon 305-764, Republic of Korea
3. National Institute of Science and Technology, Gaithersburg, Maryland 20899
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5742
Reference23 articles.
1. Measured lengths of supersonic hydrogen-air jet flames—Compared to subsonic flame lengths—and analysis
2. Blowout Stability Limits Of a Hydrogen Jet Flame In a Supersonic, Heated, Coflowinq Air Stream
3. Shock-wave-enhancement of the mixing and the stability limits of supersonic hydrogen-air jet flames
4. Measured supersonic flame properties - Heat-release patterns, pressure losses, thermal choking limits
5. 5Huh, H. “An Experimental Study of Supersonic Hydrogen-Air Flames for Scramjet Applications,” Ph.D. Dissertation, Dept. of Aerospace Engineering,Univ. of Michigan, Ann Arbor, MI,Oct. 1996.
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