Integrated Aero- Servo- Thermo- Propulso- Elasticity (ASTPE) Methodology for Hypersonic Scramjet Vehicle Design/Analysis

机译：用于超音速超燃冲压发动机飞行器设计/分析的集成航空-伺服-热-推进-弹性（ASTPE）方法

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来源
《AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition》|2010年|1-23|共23页
会议地点 Orlando FL(US)
作者
R. Starkey; D. Liu; P. Chen; A. Sengupta; K. Chang; F. Rankins;
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University of Colorado Boulder CO;

ZONA Technology Inc. Scottsdale AZ;

University of Maryland College Park MD;

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3. Scramjet Operation Guaranteed Longitudinal Control of Air-Breathing Hypersonic Vehicles [J] . Hao An, Qianqian Wu, Changhong Wang, Mechatronics, IEEE/ASME Transactions on . 2020,第6期

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4. Integrated Aero- Servo- Thermo- Propulso- Elasticity (ASTPE) Methodology for Hypersonic Scramjet Vehicle Design/Analysis [C] . American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition . 2010

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5. Combustion Efficiency, Flameout Operability Limits and General Design Optimization for Integrated Ramjet-Scramjet Hypersonic Vehicles [D] . Mbagwu, Chukwuka Chijindu. 2017

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6. Unconventionally Designed Tracking Loop Adaptable to Plasma Sheath Channel for Hypersonic Vehicles [O] . Lei Shi, Shurong Yuan, Bo Yao 2021

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7. Control-Relevant Modeling, Analysis, and Design for Scramjet-Powered Hypersonic Vehicles [O] . Dickeson Jeffrey J., Rodriguez Armando A., Benavides Jose, 2009

机译：超燃冲压发动机超音速飞行器的与控制相关的建模，分析和设计

Integrated Aero- Servo- Thermo- Propulso- Elasticity (ASTPE) Methodology for Hypersonic Scramjet Vehicle Design/Analysis

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