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RAMJET TECHNOLOGY Section on Flow Processes and Engine Performance Chapter 2 Basic Adiabatic Theory

机译：RamJET技术流程和发动机性能部分第2章基本绝热理论

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ONE-DIMENSIONAL GAS DYNAMICSn2.tTWO-DIMENSIONAL SUPERSONIC WAVE SYSTEMSn3.tTHE THRUST-PRODUCING CYCLE

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E. A. Bunt;
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年度 1964
页码 1-94
总页数 94
原文格式 PDF
正文语种 eng
中图分类工业技术;
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4. Analysis of Thermogasdynamic Processes in Using Methane in Rocket-ramjet Engines and Their Effect on Thrust-flow Performance [C] . Valery I. Timoshenko, S. Belotserkovets International Symposium on Air Breathing Engines . 2005

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5. Effects of incomplete fuel-air mixing on the performance characteristics of mixed compression, shock-induced combustion ramjet (shcramjet) engines. [D] . Redford, Tim. 1998

机译：燃料-空气不完全混合对混合压缩，冲击诱导的燃烧冲压发动机（shcramjet）发动机性能特性的影响。
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7. COLD FLOW PERFORMANCE OF A RAMJET ENGINE [O] . Harrison G Sykes -1

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8. Ramjet Technology. Section on Flow Processes and Engine Performance. Chapter 5. Combustor Flow and Engine Perofrmance [R] . Bader, F., Bunt, E. A. 1967

机译：冲压喷射技术。流程和发动机性能部分。第5章燃烧室流量和发动机性能

RAMJET TECHNOLOGY Section on Flow Processes and Engine Performance Chapter 2 Basic Adiabatic Theory

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