Impulse Generation by an Open Shock Tube
Author:
Affiliation:
1. University of Tsukuba, Tsukuba 305-8573, Japan
2. California Institute of Technology, Pasadena, California 91125
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.27467
Reference22 articles.
1. Pulse detonation propulsion: challenges, current status, and future perspective
2. Reactive impulse from the explosion of a gas mixture in a semiinfinite space
3. Propulsive Performances of Pulsed Detonations
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