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Thermal Load Considerations for Detonative Combustion- Based Gas Turbine Engines

机译：基于爆炸性燃烧的燃气涡轮发动机的热负荷考虑

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《AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit》|2004年|P.1-12|共12页
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D. Paxson; H. Perkins;
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中图分类航空发动机（推进系统）;
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4. Thermal Load Considerations for Detonative Combustion- Based Gas Turbine Engines [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/Society of Automotive Engineers/American Society for Engineering Education Joint Propulsion Conference and Exhibit . 2004

机译：爆炸燃烧的燃气轮机发动机的热负荷考虑
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7. Thermal Load Considerations for Detonative Combustion-Based Gas Turbine Engines [O] . Paxson, Daniel E., Perkins, H. Douglas 2004

机译：基于爆炸性燃烧的燃气涡轮发动机的热负荷考虑
8. Thermal Load Considerations for Detonative Combustion-Based Gas Turbine Engines [R] . Paxson, D. E. , Perkins, H. D. 2004

机译：基于爆炸燃烧的燃气轮机发动机的热负荷考虑

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