, Available online ,
doi: 10.13224/j.cnki.jasp.20250031
, Available online ,
doi: 10.13224/j.cnki.jasp.20250546
2026, 41(8): 20250318.
doi: 10.13224/j.cnki.jasp.20250318
2026, 41(8): 20250025.
doi: 10.13224/j.cnki.jasp.20250025
2026, 41(8): 20250015.
doi: 10.13224/j.cnki.jasp.20250015
2026, 41(8): 20250313.
doi: 10.13224/j.cnki.jasp.20250313
2026, 41(8): 20250022.
doi: 10.13224/j.cnki.jasp.20250022
2026, 41(8): 20250307.
doi: 10.13224/j.cnki.jasp.20250307
2026, 41(8): 20240781.
doi: 10.13224/j.cnki.jasp.20240781
2026, 41(8): 20250324.
doi: 10.13224/j.cnki.jasp.20250324
2026, 41(8): 20250335.
doi: 10.13224/j.cnki.jasp.20250335
2026, 41(7): 20240780.
doi: 10.13224/j.cnki.jasp.20240780
2026, 41(7): 20250013.
doi: 10.13224/j.cnki.jasp.20250013
2026, 41(7): 20240676.
doi: 10.13224/j.cnki.jasp.20240676
2026, 41(7): 20240664.
doi: 10.13224/j.cnki.jasp.20240664
2026, 41(7): 20250239.
doi: 10.13224/j.cnki.jasp.20250239
2026, 41(7): 20240665.
doi: 10.13224/j.cnki.jasp.20240665
2026, 41(7): 20250237.
doi: 10.13224/j.cnki.jasp.20250237
2026, 41(7): 20250158.
doi: 10.13224/j.cnki.jasp.20250158
2026, 41(6): 20240660.
doi: 10.13224/j.cnki.jasp.20240660
2026, 41(6): 20240659.
doi: 10.13224/j.cnki.jasp.20240659
2026, 41(6): 20250235.
doi: 10.13224/j.cnki.jasp.20250235
2026, 41(6): 20240646.
doi: 10.13224/j.cnki.jasp.20240646
2026, 41(6): 20240771.
doi: 10.13224/j.cnki.jasp.20240771
2026, 41(6): 20240545.
doi: 10.13224/j.cnki.jasp.20240545
2026, 41(6): 20250160.
doi: 10.13224/j.cnki.jasp.20250160
2026, 41(6): 20240657.
doi: 10.13224/j.cnki.jasp.20240657
2026, 41(6): 20240558.
doi: 10.13224/j.cnki.jasp.20240558
2026, 41(6): 20240775.
doi: 10.13224/j.cnki.jasp.20240775
Volume 41 Issue 5 2026
Display Method:
2026, 41(5): 20250197.
doi: 10.13224/j.cnki.jasp.20250197
2026, 41(5): 20250203.
doi: 10.13224/j.cnki.jasp.20250203
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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- 4 TRANSIENT OPERATING LINE INDICATOR AND ITS APPLICATION 10474
- 5 AN EXPERIMENTAL STUDY ON A LOBED NOZZLE OF AN INFRARED SUPPRESSION SYSTEM 10079
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- 2 Sample points reused failure response curve method for structural reliability analysis 8721
- 3 Numerical study on characteristics of temperature reduction and flow loss in radial pre-swirl system 7067
- 4 Combustion instability at end of burning in a solid rocket motor 6683
- 5 Component-level modeling technology for variable cycle engine 4436
- 1 Application of convolutional neural network and kurtosis in fault diagnosis of rolling bearing 116
- 2 Researches on metal rubber mechanics properties in retrospect and prospect 109
- 3 Review on shape memory alloys’ application in field of aerospace 96
- 4 Damage mechanics-finite element method for contact fatigue life prediction of ball bearings 77
- 5 Recognition of gearbox operation fault state based on CWT-CNN 74


