Thermal buckling of axially precompressed cylindrical shells irradiated bylaser beam

Citation
Ks. Deng et al., Thermal buckling of axially precompressed cylindrical shells irradiated bylaser beam, AIAA J, 38(10), 2000, pp. 1789-1794
Citations number
18
Categorie Soggetti
Aereospace Engineering
Journal title
AIAA JOURNAL
ISSN journal
00011452 → ACNP
Volume
38
Issue
10
Year of publication
2000
Pages
1789 - 1794
Database
ISI
SICI code
0001-1452(200010)38:10<1789:TBOAPC>2.0.ZU;2-H
Abstract
When a powerful laser beam irradiates a thin-walled missile structure, the temperature of the irradiated region increases rapidly, which results in co mpressive thermal stresses being developed together with softening of the s hell wall. Theoretical predictions of the buckling resistance of isotropic plates and shells, subjected to axial compression loading and a laser-induc ed nonuniform temperature field, have been developed and are presented, Mat erial properties are assumed to be temperature dependent, which results in the thermal-buckling behavior being nonlinear with respect to temperature. Theoretical predictions are presented for a cylindrical shell subjected to axial compression loading and irradiated by a powerful laser beam. These sh ow that the buckling resistance was significantly reduced hy the combined a ction of axial compression loading and laser irradiation. Hence, it is like ly that sudden buckling-induced failure may occur that can cause failure of highly optimized, lightweight cylindrical shells.