Moisture-heat effects of unidirectional composite laminates fracture toughness and fatigue crack growth

被引：0

作者：

Zhang, Fusheng ^{[1
]}

Pzinz, R. ^{[1
]}

Zichy, J.H. ^{[1
]}

机构：

[1] Beijing Univ of Aeronautics and, Astronautics, Beijing, China

来源：

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 1993年 / 02期

关键词：

Composite materials;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：7 / 15

共 50 条

[41] Translaminar notch fracture toughness expressions for composite laminates
Torabi, A. R.
Pirhadi, E.
THEORETICAL AND APPLIED FRACTURE MECHANICS, 2022, 119
[42] Stress intensity factors as the fracture parameters for delamination crack growth in composite laminates
Georgia Inst of Technology, Atlanta, United States
Composites Part B: Engineering, 1997, 28 B (04): : 375 - 384
[43] Stress intensity factors as the fracture parameters for delamination crack growth in composite laminates
Chow, WT
Atluri, SN
COMPOSITES PART B-ENGINEERING, 1997, 28 (04) : 375 - 384
[44] Fatigue crack growth rate of Ti-6Al-4V considering the effects of fracture toughness and crack closure
Junhong Zhang
Shuo Yang
Jiewei Lin
Chinese Journal of Mechanical Engineering, 2015, 28 : 409 - 415
[45] Fatigue Crack Growth Rate of Ti-6Al-4V Considering the Effects of Fracture Toughness and Crack Closure
ZHANG Junhong
YANG Shuo
LIN Jiewei
Chinese Journal of Mechanical Engineering, 2015, 28 (02) : 409 - 415
[46] Fatigue Crack Growth Rate of Ti-6Al-4V Considering the Effects of Fracture Toughness and Crack Closure
Zhang Junhong
Yang Shuo
Lin Jiewei
CHINESE JOURNAL OF MECHANICAL ENGINEERING, 2015, 28 (02) : 409 - 415
[47] TOUGHNESS CRITERION IDENTIFICATION FOR EDGE-NOTCHED UNIDIRECTIONAL COMPOSITE LAMINATES
HAUG, E
DEROUVRAY, A
COMPUTERS & STRUCTURES, 1985, 20 (1-3) : 413 - 430
[48] Fatigue Crack Growth Rate of Ti-6Al-4V Considering the Effects of Fracture Toughness and Crack Closure
ZHANG Junhong
YANG Shuo
LIN Jiewei
Chinese Journal of Mechanical Engineering, 2015, (02) : 409 - 415
[49] Stress intensity factors as the fracture parameters for delamination crack growth in composite laminates
W. T. Chow
S. N. Atluri
Computational Mechanics, 1998, 21 : 1 - 10
[50] Stress intensity factors as the fracture parameters for delamination crack growth in composite laminates
Chow, WT
Atluri, SN
COMPUTATIONAL MECHANICS, 1998, 21 (01) : 1 - 10

← 1 2 3 4 5 →