Failure models for composite structures under compression loading (2011)
- Authors:
- USP affiliated authors: TITA, VOLNEI - EESC ; RIBEIRO, MARCELO LEITE - EESC
- Unidade: EESC
- Subjects: DANOS MECÂNICOS; MATERIAIS COMPÓSITOS; ENGENHARIA AERONÁUTICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher: ABCM
- Publisher place: Rio de Janeiro, RJ
- Date published: 2011
- Source:
- Título: Proceedings of COBEM
- ISSN: 2176-5480
- Conference titles: International Congress of Mechanical Engineering - COBEM
-
ABNT
RIBEIRO, Marcelo Leite e VANDEPITTE, Dirk e TITA, Volnei. Failure models for composite structures under compression loading. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. . Acesso em: 28 dez. 2025. -
APA
Ribeiro, M. L., Vandepitte, D., & Tita, V. (2011). Failure models for composite structures under compression loading. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. -
NLM
Ribeiro ML, Vandepitte D, Tita V. Failure models for composite structures under compression loading. Proceedings of COBEM. 2011 ;[citado 2025 dez. 28 ] -
Vancouver
Ribeiro ML, Vandepitte D, Tita V. Failure models for composite structures under compression loading. Proceedings of COBEM. 2011 ;[citado 2025 dez. 28 ] - A finite element damage model to predict failure behavior of composite sandwich structures
- Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage
- Progressive failure analysis of filament wound composite tubes under internal pressure
- Influence of stacking sequence on the radial compression of filament wound composite tubes
- Experimental methodology for testing metal-composite bolted joints
- Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses
- Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression
- Unified formulation for composite plate structures: implementation and evaluation
- Analysis of delamination of composite laminates via XFEM based on the layerwise displacement theory and cohesive zone method
- A computational framework for predicting onset and crack propagation in composite structures via extended Finite Element Method (XFEM)
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
