THERMALLY INDUCED STRESSES AND DEFORMATIONS IN ANGLE-PLY COMPOSITE TUBES

被引:33
作者
HYER, MW [1 ]
ROUSSEAU, CQ [1 ]
机构
[1] GE CO,AIRCRAFT ENGINE BUSINESS GRP,CINCINNATI,OH 45215
关键词
D O I
10.1177/002199838702100504
中图分类号
TB33 [复合材料];
学科分类号
摘要
引用
收藏
页码:454 / 480
页数:27
相关论文
共 15 条
[1]  
BIRGER BI, 1971, IZVESTIYA VUZ AVIATS, V14, P24
[2]  
CHRISTENSEN RM, 1979, MECHANICS COMPOSITE
[3]  
COHEN D, 1984, 16TH SAMPE TECHN C, P577
[4]   STRESSES AND DEFORMATIONS IN CROSS-PLY COMPOSITE TUBES SUBJECTED TO A UNIFORM TEMPERATURE-CHANGE [J].
HYER, MW ;
COOPER, DE ;
COHEN, D .
JOURNAL OF THERMAL STRESSES, 1986, 9 (02) :97-117
[5]   GEOMETRIC DESIGN OF COMPOSITE CYLINDRICAL CHARACTERIZATION SPECIMENS [J].
PAGANO, NJ ;
WHITNEY, JM .
JOURNAL OF COMPOSITE MATERIALS, 1970, 4 :360-&
[6]   STRESS GRADIENTS IN LAMINATED COMPOSITE CYLINDERS [J].
PAGANO, NJ .
JOURNAL OF COMPOSITE MATERIALS, 1971, 5 (APR) :260-&
[7]  
PAGANO NJ, 1973, ASTM STP, V521, P255
[8]  
Pawlik P, 1980, ELASTICITY THEORY AP
[9]   A FINITE ELEMENT ANALYSIS OF LAMINATED ANISOTROPIC TUBES .1. CHARACTERIZATION OF OFF-AXIS TENSILE SPECIMEN [J].
RIZZO, RR ;
VICARIO, AA .
JOURNAL OF COMPOSITE MATERIALS, 1970, 4 :344-&
[10]  
RIZZO RR, 1972, ASTM STP, V497, P68