Impact Damage Analysis of Layered Composite Plates (CROSBI ID 495369)
Prilog sa skupa u zborniku | izvorni znanstveni rad | međunarodna recenzija
Podaci o odgovornosti
Smojver, Ivica ; Sorić, Jurica
engleski
Impact Damage Analysis of Layered Composite Plates
Material and geometrical parameters affecting structural response of impacted aircraft structures have been defined. Numerical model for the prediction of damage in layered composite panels under low velocity impact has been presented. The model takes into account matrix cracks and delaminations. All necessary numerical procedures have been performed within the frame of ABAQUS finite element software with the addition of user subroutines. Numerical effectiveness of the method has been demonstrated by the example of impact on the carbon/epoxy simply supported square plate [04 / 908 /04].
Finite Element Method; Layered Composites; Impact Damage; Delaminations
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Podaci o prilogu
1255-1260-x.
2002.
objavljeno
Podaci o matičnoj publikaciji
Proceedings of the 7th International Design Conference DESIGN 2002
Marjanović, Dorian
Zagreb: Fakultet strojarstva i brodogradnje Sveučilišta u Zagrebu
Podaci o skupu
7th International Design Conference DESIGN 2002
predavanje
14.05.2002-17.05.2002
Dubrovnik, Hrvatska