STRENGTH PREDICTIONS OF COMPOSITE LAMINATES WITH UNLOADED FASTENER HOLES - COMMENT

被引：0

|

作者：

PRABHAKARAN, R

机构：

来源：

AIAA JOURNAL | 1981年 / 19卷 / 10期

关键词：

D O I：

10.2514/3.60072

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

收藏

页码：1375 / 1375

页数：1

相关论文

共 50 条

[31] DESIGNING FOR TOLERANCE TO IMPACT DAMAGE AT FASTENER HOLES IN GRAPHITE EPOXY LAMINATES UNDER COMPRESSION
JANARDHANA, MN
BROWN, KC
JONES, R
THEORETICAL AND APPLIED FRACTURE MECHANICS, 1986, 5 (01) : 51 - 55
[32] Fatigue progressive damage analysis of single fastener joints in composite laminates
Institute 53, China North Group Corporation, Jinan 250031, China
不详
Fuhe Cailiao Xuebao, 2008, 1 (173-179):
[33] ANALYSIS OF CREEP AND RELAXATION IN COMPOSITE LAMINATES WITH HOLES
HWANG, IH
LIN, KY
AIAA/ASME/ASCE/AHS/ASC 30TH STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE, PTS 1-4: A COLLECTION OF TECHNICAL PAPERS, 1989, : 2064 - 2070
[34] STUDY OF THE ONSET OF DELAMINATION AT HOLES IN COMPOSITE LAMINATES
SHALEV, D
REIFSNIDER, KL
JOURNAL OF COMPOSITE MATERIALS, 1990, 24 (01) : 42 - 71
[35] NON-DESTRUCTIVE INSPECTION OF FASTENER HOLES IN GRAPHITE COMPOSITE STRUCTURES
SHELDON, WH
SOUDER, CW
MATERIALS EVALUATION, 1980, 38 (02) : S11 - S11
[36] SUPERPOSITION OF THE NOTCHED STRENGTH OF COMPOSITE LAMINATES
PIPES, RB
GILLESPIE, JW
WETHERHOLD, RC
JOURNAL OF RHEOLOGY, 1980, 24 (06) : 886 - 887
[37] Residual strength model for composite laminates
边文凤
郭景哲
杜善义
Journal of Harbin Institute of Technology(New series), 2010, (03) : 424 - 426
[38] MACROSCOPIC DESCRIPTION OF THE STRENGTH OF COMPOSITE LAMINATES
BALASUBRAMANIAN, N
CURRENT SCIENCE, 1983, 52 (24): : 1171 - 1176
[39] FATIGUE AND RESIDUAL STRENGTH OF COMPOSITE LAMINATES
ROTEM, A
ENGINEERING FRACTURE MECHANICS, 1986, 25 (5-6) : 819 - 827
[40] SUPERPOSITION OF THE NOTCHED STRENGTH OF COMPOSITE LAMINATES
PIPES, RB
GILLESPIE, JW
WETHERHOLD, RC
POLYMER ENGINEERING AND SCIENCE, 1979, 19 (16): : 1151 - 1155

← 1 2 3 4 5 →