Simulating progressive damage of notched composite laminates with various lamination schemes

• Autorzy: Mandal B. , Chakrabarti A.

Identyfikatory

DOI

10.1515/ijame-2017-0020

• Języki publikacji: EN

Abstrakty

EN

A three dimensional finite element based progressive damage model has been developed for the failure analysis of notched composite laminates. The material constitutive relations and the progressive damage algorithms are implemented into finite element code ABAQUS using user-defined subroutine UMAT. The existing failure criteria for the composite laminates are modified by including the failure criteria for fiber/matrix shear damage and delamination effects. The proposed numerical model is quite efficient and simple compared to other progressive damage models available in the literature. The efficiency of the present constitutive model and the computational scheme is verified by comparing the simulated results with the results available in the literature. A parametric study has been carried out to investigate the effect of change in lamination scheme on the failure behaviour of notched composite laminates.

Słowa kluczowe

EN

damage mechanics; user-defined subroutine; composite laminates; finite element; strength; degradation

PL

mechanika uszkodzeń; laminaty kompozytowe; wytrzymałość materiałów

• Wydawca: Oficyna Wydawnicza Uniwersytetu Zielonogórskiego
• Czasopismo: International Journal of Applied Mechanics and Engineering
• Rocznik: 2017
• Tom: Vol. 22, no. 2
• Strony: 333--347
• Opis fizyczny: Bibliogr. 16 poz., rys., tab., wykr.

Twórcy

autor

Mandal B.

• Department of Civil Engineering Indian Institute of Technology Roorkee Roorkee-247 667, INDIA

autor

Chakrabarti A.

• Department of Civil Engineering Indian Institute of Technology Roorkee Roorkee-247 667, INDIA

Bibliografia

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