Design of an Actively Valved and Acoustically Resonant Pulse Combustor for Pressure-gain Combustion Applications
Author:
Affiliation:
1. King Abdullah University of Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0899
Reference22 articles.
1. Aerodynamics
2. R. Tom Sawyer Award Lecture: Reflections on United Kingdom Aircraft Gas Turbine History
3. Influence of Unsteadiness on the Analysis of Pressure Gain Combustion Devices
4. Performance Analysis of an Ejector Enhanced Pressure Gain Combustion Gas Turbine
5. Potential Benefits to Commercial Propulsion Systems from Pressure Gain Combustion
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