Journal of Projectiles, Rockets, Missiles and Guidance >
Performance Analysis of an Aircraft with ATR Engine
Received date: 2011-04-07
Online published: 2025-05-30
The air-turbo-ramjet engine (ATR) is a kind of combined air-breathing engine with the characters of broad velocity and altitude envelope. the application characters of ATR engine, the ATR engine with the turbofan engine their propulsion characters and basic flight performances of a certain aircraft platform. The results axial-overload and economic-climb-rate etc obtained. The results show that ATR engine can upgrade the aircraft maneuverabilit and flight envelope.
Key words: ATR engine; turbofan engine; maneuverability; flight envelope
LI Ping , LIU Chang'an , HE Guoqiang , NAN Xiangyi . Performance Analysis of an Aircraft with ATR Engine[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(6) : 173 -175 . DOI: 10.15892/j.cnki.djzdxb.2011.06.031
| [1] | 陈湘, 陈玉春, 屠秋野,等. 空气涡轮火箭发动机的性能研究[J]. 弹箭与制导学报, 2009, 29(2): 162-165. |
| [2] | 张蒙正, 李平, 陈祖奎. 组合循环动力系统面临的挑战及前景[J]. 火箭推进, 2009, 35(1): 1-8. |
| [3] | 王永寿. 小型高推力空气涡轮冲压发动机[J]. 飞航导弹, 2003(5): 44-48. |
| [4] | 南向谊, 王拴虎, 李平. 空气涡轮火箭发动机研究的进展及展望[J]. 火箭推进, 2008, 34(6): 31-35. |
| [5] | 金长江, 范立钦, 周士林. 飞行力学:飞机飞行性能计算[M]. 北京: 国防工业出版社, 1990. |
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