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Dynamic Buckling of Composite Shells
Details
This thesis is focused on the investigation of the changes in the buckling behaviour of various composite shells due to dynamic, rapid loading. Currently, the structural design procedures of lightweight structures incorporate assumption of the loads as quasistatic, while maintaining reliability by applying conservative safety coefficients. Different investigations show that in various cases of dynamic loading the buckling loads can be both higher and lower than the static buckling load. Therefore, correct consideration of the load dynamics in the design procedure would lead to safer and more efficient structures. A reliable, experimentally validated analysis approach is required in order to benefit from the weight-saving potential of dynamically loaded composite structures, while maintaining the reliability. However, only few experimental investigations on dynamic buckling of composite structures have been performed because of the complexity of such experiments. In present thesis, the dynamic buckling of composite shells has been investigated experimentally and numerically, and an appropriate experimentally validated modelling approach has been proposed.
Autorentext
Edgars Eglitis was born on June 7, 1984 in Riga, Latvia. He completed the B.S. degree in civil engineering in 2005 and the M.S. degree in 2007 at Riga Technical University. While Ph.D. student, he was working as a researcher for EC 6th Framework projects ALCAS and COCOMAT. The presented PhD thesis was defended on 23th of March, 2011.
Weitere Informationen
- Allgemeine Informationen
- Sprache Englisch
- Anzahl Seiten 168
- Herausgeber LAP LAMBERT Academic Publishing
- Gewicht 268g
- Untertitel Behaviour of Plain and Stiffened Composite Shells Under Axial Pulse Loadings
- Autor Edgars Eglitis
- Titel Dynamic Buckling of Composite Shells
- Veröffentlichung 07.03.2011
- ISBN 3844313168
- Format Kartonierter Einband
- EAN 9783844313161
- Jahr 2011
- Größe H220mm x B150mm x T11mm
- GTIN 09783844313161