Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (11): 529021-529021.doi: 10.7527/S1000-6893.2023.29021
• Articles • Previous Articles
Liang MENG1,2,3, Jing ZHANG1,2, Yadong WANG1,2, Yang YU4, Fan ZHANG4, Jihong ZHU1,2,3, Weihong ZHANG1,2,3()
Received:
2023-05-19
Revised:
2023-06-14
Accepted:
2023-07-05
Online:
2023-10-11
Published:
2023-10-08
Contact:
Weihong ZHANG
E-mail:zhangwh@nwpu.edu.cn
Supported by:
CLC Number:
Liang MENG, Jing ZHANG, Yadong WANG, Yang YU, Fan ZHANG, Jihong ZHU, Weihong ZHANG. Lightweight design of stiffening ribs layout of a bypass engine casing[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(11): 529021-529021.
Table 5
Comparison of critical buckling loads of stiffened bypass engine casing under different conditions
加筋构型 | 轴向压力/N | 弯矩/(N∙m) | 扭矩/(N∙m) | 外部压强/MPa |
---|---|---|---|---|
矩形加筋 | 4.91×105 | 9.55×104 | 1.36×105 | 0.199 |
斜置正交加筋 | 4.44×105 | 8.70×104 | 1.51×105 | 0.204 |
三角形加筋 | 4.06×105 | 8.05×104 | 1.51×105 | 0.217 |
六边形加筋 | 5.95×105 | 11.5×104 | 1.12×105 | 0.133 |
三角形加筋 屈曲模态 | ||||
失效模式 | 局部屈曲 | 局部屈曲 | 整体屈曲 | 整体屈曲 |
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