Unsteady Performance of Rotating Detonation Engines with Different Exhaust Nozzles
Author:
Affiliation:
1. Purdue University, West Lafayette, Indiana 47907
2. von Kármán Institute for Fluid Dynamics, 1640 Sint-Genesius-Rode, Belgium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B36164
Reference32 articles.
1. Detailed structure of spinning detonation in a circular tube
2. Numerical investigation of flow particle paths and thermodynamic performance of continuously rotating detonation engines
3. Continuous Detonation Engine and Effects of Different Types of Nozzle on Its Propulsion Performance
4. Thermodynamic Cycle Analysis of Pulse Detonation Engines
5. Experimental proof of the energy efficiency of the Zel’dovich thermodynamic cycle
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