中国机械工程学会生产工程分会知识服务平台

期刊


ISSN0334-0082
刊名International Journal of Turbo and Jet Engines
参考译名国际涡轮机与喷气发动机杂志
收藏年代2000~2024



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2024

2017, vol.34, no.1 2017, vol.34, no.2 2017, vol.34, no.3 2017, vol.34, no.4

题名作者出版年年卷期
Software Development for EECU Platform of Turbofan EngineKim, Bo Gyoung; Kwak, Dohyup; Kim, Byunghyun; Choi, Hee Ju; Kong, Changduk20172017, vol.34, no.1
Analysis of Compressor Surge in a Military Turbojet Engine: A Case StudyChandel, Sunil; Mishra, R. K.; Bhat, R. Raghavendra20172017, vol.34, no.1
Influence of Structural Parameters on the Performance of Vortex Valve Variable-Thrust Solid Rocket MotorWei, Xianggeng; Li, Jiang; He, Guoqiang20172017, vol.34, no.1
Numerical Studies on the Performance of Scramjet Combustor with Alternating Wedge-Shaped Strut InjectorChoubey, Gautam; Pandey, K. M.20172017, vol.34, no.1
Investigation of HP Turbine Blade Failure in a Military Turbofan EngineMishra, R. K.; Thomas, Johny; Srinivasan, K.; Nandi, Vaishakhi; Bhatt, R. Raghavendra20172017, vol.34, no.1
Nozzle Admittance and Damping Analysis Using the LEE MethodWang Mu-xin; Liu Pei-jin; Yang Wen-jing; Wei Xiang-geng20172017, vol.34, no.1
Numerical Study of the Propulsive Performance of the Hollow Rotating Detonation Engine with a Laval NozzleYao, Songbai; Tang, Xinmeng; Wang, Jianping20172017, vol.34, no.1
The Combined Effects of Surface Roughness with Upstream Wakes on the Boundary Layer Development of an Ultra-High-Lift LPT BladeSun Shuang; Lei Zhijun; Lu Xin'gen; Zhang Yanfeng; Zhu Junqiang20172017, vol.34, no.1
Numerical Investigation of a Model Scramjet Combustor Using DDESShin, Junsu; Sung, Hong-Gye20172017, vol.34, no.1
Flow Field Measurement in Multi-stage Axial Compressor Stator by Using Multi-hole Pneumatic ProbesWang Zhiqiang; Lu Bo; Zhang Chenkai; Hu Jun20172017, vol.34, no.1
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