Test Results on the Stability and Vibrations of Composite Shells

2017
Abramovich H., Kaspars Kalniņš, Wieder A.

This chapter presents experimental results for tests being performed on various thin-walled structures (shells and cones) manufactured from either laminated composite sandwich/materials or isotropic materials (steel, aluminum). All the specimens were under axial compression and were tested till their complete collapse.

Atslēgas vārdi
Buckling, Buckling load, Cone, Initial geometric imperfection, Knockdown factor, Laminated composite layer, Sandwich, Shell, Strain gage
DOI
10.1016/B978-0-08-100410-4.00013-2
Hipersaite
https://www.sciencedirect.com/science/article/pii/B9780081004104000132?via%3Dihub

H., A., Kalniņš, K., A., W. Test Results on the Stability and Vibrations of Composite Shells. No: Stability and Vibrations of Thin Walled Composite Structures. [S.l.]: Woodhead Publishing, 2017. 619.-691.lpp. ISBN 978-0-08-100410-4. e-ISBN 978-0-08-100429-6. Pieejams: doi:10.1016/B978-0-08-100410-4.00013-2

Publikācijas valoda
English (en)