Parametric Study of Pulse-Combustor-Driven Ejectors at High-Pressure
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-4190
Reference16 articles.
1. Potential Benefits to Commercial Propulsion Systems from Pressure Gain Combustion
2. Ejector Enhanced Pulsejet Based Pressure Gain Combustors: An Old Idea With a New Twist
3. Pulse combustion: The importance of characteristic times
4. Foundational Performance Analyses of Pressure Gain Combustion Thermodynamic Benefits for Gas Turbines
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Computational Study of Compact Ejector-Enhanced Resonant Pulse Combustors;2018 Joint Propulsion Conference;2018-07-08
2. Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure;Journal of Propulsion and Power;2017-01
3. Numerical Evaluation of an Ejector-Enhanced Resonant Pulse Combustor with a Poppet Inlet Valve and a Converging Exhaust Nozzle;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22
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