Study on Buckling Behaviour of Laminated Shells under Pulse Loading

Proceedings of International Coucil of the Aeronautical Sciences 2010 Congress 2010
Edgars Eglītis, Kaspars Kalniņš, Chiara Bisagni

This experimental and numerical study focuses on the problem of buckling of cylindrical composite shells under pulse loads. Series of static and dynamic pulse buckling experiments have been performed to determine buckling loads of cylindrical composite specimens under different axial loading speeds. Numerical investigation on influence of imperfections has been carried out and the results are compared with the experimental data.

Atslēgas vārdi
dynamic buckling, buckling tests, pulse loads, composite shells, imperfections

Eglītis, E., Kalniņš, K., Bisagni, C. Study on Buckling Behaviour of Laminated Shells under Pulse Loading. No: Proceedings of International Coucil of the Aeronautical Sciences 2010 Congress, Francija, Nice, 19.-24. septembris, 2010. Nice: International Coucil of the Aeronautical Sciences, 2010, 1.-8.lpp.

Publikācijas valoda
English (en)