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Analysis of rocket, ram-jet, and turbojet engines for supersonic propulsion of long-range missiles I : rocket-engine performance

机译：用于远程导弹超音速推进的火箭，冲压喷气发动机和涡轮喷气发动机的分析I：火箭发动机性能

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Kerrebrock, Jack; Huff, Vearl N;
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年度 1954
页码 1-54
总页数 54
原文格式 PDF
正文语种 eng
中图分类工业技术;
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4. DESIGN OF AN AIR-LAUNCHED TACTICAL MISSILE FOR THREE DIFFERENT PROPULSION SYSTEMS: ATR, ROCKET AND TURBOJET [C] . Henrik Edefur, Fredrik Haglind, Stefan Olsson ASME(American Society of Mechanical Engineers) Turbo Expo vol.1; 20070514-17; Montreal(CA) . 2007

机译：三种不同的推进系统的气发射战术导弹的设计：ATR，火箭和涡轮喷气
5. Nonlinear Rocket-engine Longitudinal Combustion Instability [D] . Nguyen, Tuan Minh. 2018

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6. Hydraulic performance prediction and optimization of an engine cooling water pump using computational fluid dynamic analysis [O] . Libin Tan, Yuejin Yuan, Man Zhang 2021

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7. Flow Matching Results of an MHD Energy Bypass System on a Supersonic Turbojet Engine Using the Numerical Propulsion System Simulation (NPSS) Environment [O] . Benyo Theresa L. 2011

机译：使用数值推进系统仿真（NPSS）环境的超音速涡轮喷气发动机MHD能量旁路系统的流量匹配结果
8. Analysis of rocket, ram-jet, and turbojet engines for supersonic propulsion of long-range missiles III : ram-jet engine performance [R] . Weber, Richard J, Luidens, Roger W 1954

机译：用于远程导弹超音速推进的火箭，冲压喷气发动机和涡轮喷气发动机的分析III：冲压发动机性能

Analysis of rocket, ram-jet, and turbojet engines for supersonic propulsion of long-range missiles I : rocket-engine performance

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