, Available online ,
doi: 10.13224/j.cnki.jasp.20210722
, Available online ,
doi: 10.13224/j.cnki.jasp.20210715
, Available online ,
doi: 10.13224/j.cnki.jasp.20210219
2023, 38(3): 513-521.
doi: 10.13224/j.cnki.jasp.20220700
2023, 38(3): 522-534.
doi: 10.13224/j.cnki.jasp.20210460
2023, 38(3): 535-545.
doi: 10.13224/j.cnki.jasp.20220721
2023, 38(3): 546-557.
doi: 10.13224/j.cnki.jasp.20210462
2023, 38(3): 558-568.
doi: 10.13224/j.cnki.jasp.20220543
2023, 38(3): 588-595.
doi: 10.13224/j.cnki.jasp.20220444
2023, 38(3): 630-639.
doi: 10.13224/j.cnki.jasp.20210449
2023, 38(3): 674-684.
doi: 10.13224/j.cnki.jasp.20210452
2023, 38(3): 685-697.
doi: 10.13224/j.cnki.jasp.20210508
2023, 38(3): 698-708.
doi: 10.13224/j.cnki.jasp.20210205
2023, 38(3): 728-734.
doi: 10.13224/j.cnki.jasp.20210215
2023, 38(3): 735-742.
doi: 10.13224/j.cnki.jasp.20210720
Volume 38 Issue 2 2023
Display Method:
2023, 38(2): 257-268.
doi: 10.13224/j.cnki.jasp.20220230
2023, 38(2): 288-297.
doi: 10.13224/j.cnki.jasp.20210322
2023, 38(2): 298-311.
doi: 10.13224/j.cnki.jasp.20210199
2023, 38(2): 325-334.
doi: 10.13224/j.cnki.jasp.20210425
2023, 38(2): 335-343.
doi: 10.13224/j.cnki.jasp.20210202
2023, 38(2): 344-353.
doi: 10.13224/j.cnki.jasp.20210413
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
Top View
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- 2 TRANSIENT OPERATING LINE INDICATOR AND ITS APPLICATION 9656
- 3 DEVELOPMENT OF HIGH BY-PASS RATIO TURBOFAN ENGINES 9444
- 4 EXPERIMENTAL INVESTIGATION ON COMPRESSOR STATOR TANDEM CASCADES AT HIGH SUBSONIC SPEED 9302
- 5 AN EXPERIMENTAL STUDY ON A LOBED NOZZLE OF AN INFRARED SUPPRESSION SYSTEM 9264
- 1 Aero-engine rotor-stator rubbing positions diagnosis rule acquisition based on support vector machine 13044
- 2 Sample points reused failure response curve method for structural reliability analysis 8687
- 3 Numerical study on characteristics of temperature reduction and flow loss in radial pre-swirl system 7039
- 4 Combustion instability at end of burning in a solid rocket motor 6619
- 5 Component-level modeling technology for variable cycle engine 4315
- 1 Application of convolutional neural network and kurtosis in fault diagnosis of rolling bearing 61
- 2 Researches on metal rubber mechanics properties in retrospect and prospect 58
- 3 Aeroengine fault diagnosis based on IPSOElman neural network 46
- 4 Analysis on dynamic characteristics of high speed angular contact ball bearing based on quasi-dynamic 43
- 5 Fault diagnosis of planetary gearbox based on adaptive parameter variational mode decomposition 42