Characterization of a Premixed Laboratory Scale Pulsed Detonation Burner
Author:
Affiliation:
1. Innovative Scientific Solutions, Inc.
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1610
Reference8 articles.
1. Thermodynamic Cycle Analysis of Pulse Detonation Engines
2. The Thermodynamic Basis of Pulsed Detonation Engine Thrust Production
3. Thermodynamic Modeling of a Rotating Detonation Engine Through a Reduced Order Approach
4. Experimental Study of the Performance of a Rotating Detonation Engine with Nozzle
5. Imaging of OH* Chemiluminescence in an Optically Accessible Nonpremixed Rotating Detonation Engine
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