Increase in the hypervelocity test envelope of the HYPULSE shock-expansion tube
Author:
Affiliation:
1. General Applied Science Labs., Inc., Ronkonkoma, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2524
Reference14 articles.
1. Pulsonetti, M. and Erdos, J. "Use of an Expansion Tube to Examine Scramjct Combuslion at Hypersonic Velocities," AIAA Paper No. 89-2536,July 10-12,1989.
2. Hypersonic mixing and combustion studies in the hypulse facility
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