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Thrust Reverser for a Separate Exhaust High Bypass Ratio Turbofan Engine and its Effect on Aircraft and Engine Performance

机译：用于单独排气高旁通比涡扇发动机的推力换向器及其对飞机和发动机性能的影响

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Tashfeen Mahmood; Anthony Jackson; Vishal Sethi; Pericles Pilidis;
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1. Thrust Performance Evaluation of a Turbofan Engine Based on Exergetic Approach and Thrust Management in Aircraft [J] . Yalcin Enver International Journal of Turbo and Jet Engines . 2017,第2期

机译：基于防辐射方法的涡轮机发动机推力绩效评价与飞机推力管理
2. Review of Thrust Reverser Mechanism used in Turbofan Jet Engine Aircraft [J] . Mohd Anees Siddiqui, Md Shakibul Haq International journal of instrumentation science and engineering . 2013,第1期

机译：涡扇喷气发动机飞机推力反向器机构综述
3. Next Generation of Transport Engines-Very High Bypass Ratio Turbofans vs Open Rotor Engines [J] . Robert S Mazzawy Mechanical Engineering . 2010,第12期

机译：下一代运输发动机-超高旁路比涡轮风扇与开放式转子发动机
4. Thrust Reverser for a Separate Exhaust High Bypass Ratio Turbofan Engine and its Effect on Aircraft and Engine Performance [C] . Tashfeen Mahmood, Anthony Jackson, Vishal Sethi, ASME turbo expo . 2012

机译：单独排气高旁路比涡扇发动机的推力反向器及其对飞机和发动机性能的影响
5. The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets [D] . Cleary, Spencer. 2018

机译：高旁路比率涡发发动机与固定锥形尖峰入口的超音速性能
6. Performance and exhaust emission characteristics of variable compression ratio diesel engine fuelled with esters of crude rice bran oil [O] . Mohit Vasudeva, Sumeet Sharma, S. K. Mohapatra, -1

机译：以米糠油为原料的可变压缩比柴油机的性能和废气排放特性
7. Reverse thrust performance of the QCSEE variable pitch turbofan engine [O] . Blodmer H. E., Samanich N. E., Reemsnyder D. C. 1980

机译：QCSEE可变螺距涡扇发动机的反推性能
8. Acoustics and Thrust of Separate Flow Exhaust Nozzles With Mixing Devices Investigated for High Bypass Ratio Engines. [R] . N. H. Saiyed 2000

机译：采用混合装置分离流量排气喷嘴的声学和推力研究高旁通比发动机。

Thrust Reverser for a Separate Exhaust High Bypass Ratio Turbofan Engine and its Effect on Aircraft and Engine Performance

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