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Fundamental Analysis of a Combined Cycle Rocket- Ramjet Propulsion System

机译：联合循环火箭-冲压喷气发动机推进系统的基础分析

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《AIAA International Space Planes and Hypersonic Systems and Technologies Conference》|2008年|P.1-9|共9页
会议地点 Dayton OH(US)
作者
R. LeMoyne;
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Running Springs CA;

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4. Fundamental Analysis of a Combined Cycle Rocket- Ramjet Propulsion System [C] . AIAA International Space Planes and Hypersonic Systems and Technologies Conference . 2008

机译：结合循环火箭 - 拉姆喷嘴推进系统的根本分析
5. Reynolds-averaged Navier-Stokes analysis of the flow through a model rocket-based combined-cycle engine with an independently-fueled ramjet stream. [D] . Bond, Ryan Bomar. 2003

机译：雷诺数平均Navier-Stokes对带有独立燃料冲压发动机流的基于模型的基于火箭的联合循环发动机的流量的分析。
6. Thermodynamic Analysis of a Hybrid Power System Combining Kalina Cycle with Liquid Air Energy Storage [O] . Tong Zhang, Xuelin Zhang, Xiaodai Xue, 2019

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7. PRELIMINARY ANALYSIS OF SUPERCHARGED NUCLEAR RAMJET PROPULSION SYSTEM [O] . Boppart, J. A. 1957

机译：超级核弹射推进系统的初步分析

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