China Mechanical Engineering ›› 2026, Vol. 37 ›› Issue (2): 452-465.DOI: 10.3969/j.issn.1004-132X.2026.02.020
JIANG Xuetao, YANG Yong(
), ZHU Jihong, FENG Hao, PAN Shunyang
Received:2025-09-09
Online:2026-02-25
Published:2026-03-13
Contact:
YANG Yong
通讯作者:
杨勇
作者简介:姜学涛,男,1997年生,硕士研究生。研究方向为加筋薄壳优化设计基金资助:CLC Number:
JIANG Xuetao, YANG Yong, ZHU Jihong, FENG Hao, PAN Shunyang. Buckling Topological Design of Reinforced Plate/Shell Based on Bionic Diffusion Growth-driven Method[J]. China Mechanical Engineering, 2026, 37(2): 452-465.
姜学涛, 杨勇, 朱季红, 冯昊, 潘顺洋. 基于仿生扩散生长驱动的加筋板壳抗屈曲拓扑设计[J]. 中国机械工程, 2026, 37(2): 452-465.
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URL: https://www.cmemo.org.cn/EN/10.3969/j.issn.1004-132X.2026.02.020
| Items | k | 体积 ( | 屈曲载荷因子 ( | |
|---|---|---|---|---|
| 初始 | 0 | 0.00 | 1.5910 | 0.00 |
| Case 1(a) | 38 | +2.54 | 2.5788 | +62.09 |
| Case 1(b) | 39 | +2.54 | 2.4583 | +54.51 |
| Case 1(c) | 35 | +2.51 | 2.5506 | +60.31 |
| Case 1(d) | 40 | +2.49 | 2.7857 | +75.09 |
Tab.1 Numerical results of square plate simply supported on 4 edges(SSSS,κ=25%,ΔV¯=2.5%)
| Items | k | 体积 ( | 屈曲载荷因子 ( | |
|---|---|---|---|---|
| 初始 | 0 | 0.00 | 1.5910 | 0.00 |
| Case 1(a) | 38 | +2.54 | 2.5788 | +62.09 |
| Case 1(b) | 39 | +2.54 | 2.4583 | +54.51 |
| Case 1(c) | 35 | +2.51 | 2.5506 | +60.31 |
| Case 1(d) | 40 | +2.49 | 2.7857 | +75.09 |
| k | Case 2 | k | Case 3 | ||||||
|---|---|---|---|---|---|---|---|---|---|
| 体积( | 屈曲因子( | 体积( | 屈曲因子( | ||||||
| 初始 | 0 | 0.00 | 3.3160 | 0.00 | 初始 | 0 | 0.00 | 9.0370 | 0.00 |
| / | +5.22 | 3.8876 | +17.24 | / | +5.22 | 10.5650 | +16.91 | ||
| 15 | +0.91 | 3.8123 | +14.97 | 5 | +0.37 | 9.70220 | +7.36 | ||
| 25 | +1.53 | 4.0328 | +21.60 | 15 | +1.10 | 10.3470 | +14.50 | ||
| 50 | +4.43 | 4.5845 | +38.25 | 35 | +3.21 | 11.8090 | +30.67 | ||
| 62 | +5.17 | 4.9271 | +48.59 | 47 | +5.13 | 13.2090 | +46.17 | ||
| 25 | +1.46 | 4.0062 | +20.81 | 5 | +0.37 | 9.7022 | +7.36 | ||
| 50 | +2.84 | 4.4178 | +33.23 | 15 | +0.97 | 10.2790 | +13.74 | ||
| 75 | +4.15 | 4.8734 | +46.97 | 35 | +3.77 | 11.9580 | +33.32 | ||
| 90 | +5.06 | 5.5211 | +57.45 | 45 | +5.08 | 13.0540 | +44.45 | ||
| 25 | +1.54 | 4.0067 | +20.83 | 5 | +0.37 | 9.7010 | +7.35 | ||
| 50 | +2.94 | 4.4512 | +34.23 | 15 | +1.14 | 10.3630 | +14.67 | ||
| 75 | +4.29 | 4.8240 | +45.48 | 35 | +3.67 | 12.2990 | +36.10 | ||
| 87 | +5.02 | 5.0161 | +51.27 | 45 | +5.09 | 13.3050 | +47.23 | ||
Tab. 2 Numerical results of rectangle plate with simply supported on 4 edges(a∶b=4∶3, ΔV¯=5%)
| k | Case 2 | k | Case 3 | ||||||
|---|---|---|---|---|---|---|---|---|---|
| 体积( | 屈曲因子( | 体积( | 屈曲因子( | ||||||
| 初始 | 0 | 0.00 | 3.3160 | 0.00 | 初始 | 0 | 0.00 | 9.0370 | 0.00 |
| / | +5.22 | 3.8876 | +17.24 | / | +5.22 | 10.5650 | +16.91 | ||
| 15 | +0.91 | 3.8123 | +14.97 | 5 | +0.37 | 9.70220 | +7.36 | ||
| 25 | +1.53 | 4.0328 | +21.60 | 15 | +1.10 | 10.3470 | +14.50 | ||
| 50 | +4.43 | 4.5845 | +38.25 | 35 | +3.21 | 11.8090 | +30.67 | ||
| 62 | +5.17 | 4.9271 | +48.59 | 47 | +5.13 | 13.2090 | +46.17 | ||
| 25 | +1.46 | 4.0062 | +20.81 | 5 | +0.37 | 9.7022 | +7.36 | ||
| 50 | +2.84 | 4.4178 | +33.23 | 15 | +0.97 | 10.2790 | +13.74 | ||
| 75 | +4.15 | 4.8734 | +46.97 | 35 | +3.77 | 11.9580 | +33.32 | ||
| 90 | +5.06 | 5.5211 | +57.45 | 45 | +5.08 | 13.0540 | +44.45 | ||
| 25 | +1.54 | 4.0067 | +20.83 | 5 | +0.37 | 9.7010 | +7.35 | ||
| 50 | +2.94 | 4.4512 | +34.23 | 15 | +1.14 | 10.3630 | +14.67 | ||
| 75 | +4.29 | 4.8240 | +45.48 | 35 | +3.67 | 12.2990 | +36.10 | ||
| 87 | +5.02 | 5.0161 | +51.27 | 45 | +5.09 | 13.3050 | +47.23 | ||
| k | 体积( | 屈曲因子( | ||
|---|---|---|---|---|
| 初值 | 0 | 0.00 | 0.4848 | 0.00 |
图19 Case 4 | 25 | +0.79 | 0.5854 | +20.76 |
| 50 | +1.44 | 0.6491 | +33.88 | |
| 75 | +2.09 | 0.6889 | +42.10 | |
| 100 | +3.12 | 0.8069 | +66.44 | |
| 108 | +3.51 | 0.8114 | +67.36 | |
Tab.3 Result of rectangle plate with simply supported on ane edge under unilateral axial pressure (a∶b=2∶1 with SFSF BC condition)
| k | 体积( | 屈曲因子( | ||
|---|---|---|---|---|
| 初值 | 0 | 0.00 | 0.4848 | 0.00 |
图19 Case 4 | 25 | +0.79 | 0.5854 | +20.76 |
| 50 | +1.44 | 0.6491 | +33.88 | |
| 75 | +2.09 | 0.6889 | +42.10 | |
| 100 | +3.12 | 0.8069 | +66.44 | |
| 108 | +3.51 | 0.8114 | +67.36 | |
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