Reaction Ratio and Nozzle Expansion Effects on the PDE
Author:
Affiliation:
1. Boeing - Phantom Works
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4514
Reference12 articles.
1. Integrated Vehicle Comparison of Turbo-Ramjet Engine and Pulsed Detonation Engine (PDE)
2. Thermodynamic Cycle Analysis of Pulse Detonation Engines
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