CENTRAL AND NONCENTRAL NORMAL IMPACT ON ORTHOTROPIC - COMPOSITE CYLINDRICAL-SHELLS

Citation
Sw. Gong et al., CENTRAL AND NONCENTRAL NORMAL IMPACT ON ORTHOTROPIC - COMPOSITE CYLINDRICAL-SHELLS, AIAA journal, 34(8), 1996, pp. 1619-1626
Citations number
12
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00011452
Volume
34
Issue
8
Year of publication
1996
Pages
1619 - 1626
Database
ISI
SICI code
0001-1452(1996)34:8<1619:CANNIO>2.0.ZU;2-5
Abstract
The response of orthotropic composite cylindrical shells subjected to low-velocity impact by a solid striker is described. An analytical sol ution that accommodates normal impact at any location is presented. Th is solution is based on a higher order shear deformation theory and de rived in terms of two sets of shell coordinates and an integer factor to facilitate analysis of noncentral impact. An analytic impact force function recently proposed by the authors is used to predict the conta ct force between striker and shell and this is incorporated into the s olution. Impact experiments are also conducted on a simply supported g lass/epoxy cylindrical shell. The effective contact stiffness between the shell and striker is obtained by fitting an impact force function to experimental data. The strain responses of the shell to central and noncentral impact are investigated and the present solutions verified by the experiments.