High-Speed Schlieren and Particle Image Velocimetry of the Exhaust Flow of a Pulse Detonation Combustor
Author:
Affiliation:
1. Technical University of Berlin, D-10623 Berlin, Germany
2. Monash University, Clayton, Victoria 3800, Australia
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference47 articles.
1. Recent Developments in the Research on Rotating-Detonation-Wave Engines
2. Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure
3. Review on Recent Advances in Pulse Detonation Engines
4. Detonative propulsion
5. Experimental Investigations of the Performance of a Multitube Pulse Detonation Turbine System
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