Assessment of the Performance of a Pulsejet and Comparison with a Pulsed-Detonation Engine
Author:
Affiliation:
1. Air Force Research Laboratory
2. NASA Glenn Research Center
3. Innovative Scientific Solutions Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-228
Reference14 articles.
1. Thermodynamic Cycle Analysis of Pulse Detonation Engines
2. Kentfield,J.A.C.,Nonsteady,One-Dimensional,Internal,CompressibleFlows,OxfordUniversityPress,1993.pp.191-235.
3. Pulse combustion
4. Quinn, D. D., and Paxson, D. E. "A Simplified Model for Investigation of Acoustically Driven Combustion Instabilities," AIAAPaper 1998-3764,July1998.
5. A Numerical Investigation of Premixed Combustion in Wave Rotors
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