Wave Implosion as an Initiation Mechanism for Pulse Detonation Engines
Author:
Affiliation:
1. California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4820
Reference41 articles.
1. Effects of ignition characteristics and geometry on the performance of a JP-10/O2 fueled pulse detonation engine
2. Initiator performance for liquid-fueled pulse detonation engines
3. On the propagation of shock waves through regions of non-uniform area or flow
4. Cylindrical Imploding Shock Waves
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3. Determination of Practical Computational Cell Size for Simulation of H2 Air Detonations in Pulse Detonation Engines;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
4. Research on Pulse Detonation Combustion Systems: A Status Report;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
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