Founded in 1986, monthly
Sponsor: Aviation Industry Corporation of China
Sponsored by: Chinese Society of Aeronautics Beijing University of Aeronautics and Astronautics
ISSN: 1000-8055
CN: 11-2297/V
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More+- 1 Prospects of the Aeroengine Control Development in the Early Time of the 21st Century 11197
- 2 TRANSIENT OPERATING LINE INDICATOR AND ITS APPLICATION 9783
- 3 DEVELOPMENT OF HIGH BY-PASS RATIO TURBOFAN ENGINES 9608
- 4 EXPERIMENTAL INVESTIGATION ON COMPRESSOR STATOR TANDEM CASCADES AT HIGH SUBSONIC SPEED 9429
- 5 AN EXPERIMENTAL STUDY ON A LOBED NOZZLE OF AN INFRARED SUPPRESSION SYSTEM 9346
- 1 Aero-engine rotor-stator rubbing positions diagnosis rule acquisition based on support vector machine 13128
- 2 Sample points reused failure response curve method for structural reliability analysis 8702
- 3 Numerical study on characteristics of temperature reduction and flow loss in radial pre-swirl system 7048
- 4 Combustion instability at end of burning in a solid rocket motor 6652
- 5 Component-level modeling technology for variable cycle engine 4369
- 1 Application of convolutional neural network and kurtosis in fault diagnosis of rolling bearing 89
- 2 Researches on metal rubber mechanics properties in retrospect and prospect 80
- 3 Aeroengine fault diagnosis based on IPSOElman neural network 57
- 4 Fault diagnosis of planetary gearbox based on adaptive parameter variational mode decomposition 57
- 5 Analysis on dynamic characteristics of high speed angular contact ball bearing based on quasi-dynamic 56