000004726 001__ 4726
000004726 005__ 20141119144548.0
000004726 04107 $$aeng
000004726 046__ $$k2002-06-02
000004726 100__ $$aMobasher, Barzin
000004726 24500 $$aMECHANICAL MODELING OF GLASS AND CARBON EPOXY COMPOSITES

000004726 24630 $$n15.$$pProceedings of the 15th ASCE Engineering Mechanics Division Conference
000004726 260__ $$bColumbia University in the City of New York
000004726 506__ $$arestricted
000004726 520__ $$2eng$$aA Theoretical model to predict the response of laminated composites is developed. The micromechanical model simulates the mechanical response of a multi layer composite laminate under uniaxial, biaxial, and flexural loading modes. The stacking sequence is utilized to obtain the overall stiffness matrix for each lamina. Effect of distributed cracking on the stiffness degradation of the cross ply layers under tensile loading is measured using a scalar damage parameter. The model is calibrated by predicting the ultimate strength of unidirectional, cross ply, and angle ply laminates under tensile and flexural loading.

000004726 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000004726 653__ $$a

000004726 7112_ $$a15th ASCE Engineering Mechanics Division Conference$$cNew York (US)$$d2002-06-02 / 2002-06-05$$gEM2002
000004726 720__ $$aMobasher, Barzin
000004726 8560_ $$ffischerc@itam.cas.cz
000004726 8564_ $$s328615$$uhttp://invenio.itam.cas.cz/record/4726/files/234.pdf$$yOriginal version of the author's contribution as presented on CD, .
000004726 962__ $$r4594
000004726 980__ $$aPAPER