Shock Transfer and Shock-Initiated Detonation in a Dual Pulse Detonation Engine/Crossover System
Author:
Affiliation:
1. School of Aerospace Systems, University of Cincinnati, Cincinnati, Ohio 45221
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053027
Reference19 articles.
1. Thermodynamic Cycle Analysis of Pulse Detonation Engines
2. Impact of DDT Mechanism, Combustion Wave Speed, Temperature, and Charge Quality on Pulsed-Detonation-Engine Performance
3. Detonation Initiation Improvements Using Swept-Ramp Obstacles
4. Propagation of Detonation Waves in Tubes Split from a PDE Thrust Tube
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