BEHAVIOR OF COMPOSITE LAMINATES AFTER INITIAL FAILURES

被引:89
作者
HAHN, HT [1 ]
TSAI, SW [1 ]
机构
[1] USAF,MAT LAB,NONMET MAT DIV,WRIGHT PATTERSON AFB,OH 45433
关键词
D O I
10.1177/002199837400800306
中图分类号
TB33 [复合材料];
学科分类号
摘要
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页码:288 / 305
页数:18
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共 26 条
[11]  
HAHN HT, AFMLTR7413 AIR FORC
[12]   STRUCTURE-PROPERTY RELATIONS AND RELIABILITY CONCEPTS [J].
HALPIN, JC .
JOURNAL OF COMPOSITE MATERIALS, 1972, 6 (APR) :208-&
[13]  
HASHIN Z, 1973, NAS111284 NASA CONT
[14]  
HAYASHI T, 1973, FUKUGO ZAIRYO, V1, P21
[15]  
KALNIN IL, 1972, STP497 ASTM, P551
[16]   A METHOD OF PRDICTING NONLINEAR BEHAVIOR OF LAMINATED COMPOSITES [J].
PETIT, PH ;
WADDOUPS, ME .
JOURNAL OF COMPOSITE MATERIALS, 1969, 3 (JAN) :2-&
[17]  
SANDHU RS, 1974, 15 AIAA STRUCT STRUC
[18]  
SANDHU RS, 1971, AFFDLTR7271 AIR FORC
[19]  
SENDECKYJ GP, 1974, APR COMP REL C LAS V
[20]  
SHLITSA RP, 1966, POLYMER MECHANICS, V2, P194