FINITE-ELEMENT ANALYSIS OF A LAMINATED COMPOSITE PLATE SUBJECTED TO CIRCULARLY DISTRIBUTED CENTRAL IMPACT LOADING

被引:31
作者
AGGOUR, H
SUN, CT
机构
[1] Univ of Florida, Gainesville, FL,, USA, Univ of Florida, Gainesville, FL, USA
关键词
COMPOSITE MATERIALS - Fiber Reinforced - LAMINATED PRODUCTS - MATHEMATICAL TECHNIQUES - Finite Element Method - STRESSES - Analysis;
D O I
10.1016/0045-7949(88)90412-9
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A two dimensional finite element analysis has been made for a fiber-reinforced composite laminate subjected to circularly distributed impact load which results, for example, from impacting the plate with a blunt-ended projectile. A finite element displacement model which includes the effects of transverse shear deformation and rotary inertia was used along with Hamilton's principle to derive the finite element matrices. Newmark's direct integration technique was used to integrate with respect to time. The interaction force between the projectile and the plate was calculated by using the Hertzian law of contact. Results for laminate deformations are shown to compare quantitatively with experimental results. Numerical values for stresses in the plate were calculated.
引用
收藏
页码:729 / 736
页数:8
相关论文
共 16 条
[1]  
AGGOUR H, 1986, THESIS U FLORIDA GAI
[2]  
Bathe K.-J., 2016, FINITE ELEMENT PROCE, V2nd
[3]  
CRISTESCU N, 1975, ASTMSTP568 ASME
[4]  
FUNG YC, 1965, F SOLID MECHANICS
[5]  
GOLDSMITH W, 1960, IMPACT THEORY PHYSIC
[6]  
MALVERN LE, 1979, HIGH VELOCITY DEFORM
[7]   A PENALTY PLATE-BENDING ELEMENT FOR THE ANALYSIS OF LAMINATED ANISOTROPIC COMPOSITE PLATES [J].
REDDY, JN .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1980, 15 (08) :1187-1206
[8]  
ROSS CA, 1976, FIBRE SCI TECHNOL, V9
[9]  
SIERAKOWSKI RL, 1976, DAAG29760085 U FLOR
[10]  
Stavsky Y., 1966, INT J SOLIDS STRUCT, V2, P665, DOI DOI 10.1016/0020-7683(66)90045-X