I need to model an aircraft door with a sandwich construction as given below.
-- Prepreg - Face skin (0/90)
-- Prepreg - Doubler (+-45)
-- Core Material
-- Prepreg - Doubler (+-45)
-- Prepreg - Face skin (0/90)
I am doing it by using 3D solid modeling for the core and 2D shell modeling for the...
Hello all,
I am trying to simulate progressive failure analysis of composites using SOL 600. I am post processing the Marc T16 file in patran for the results. I am using displacement controlled load. So I need to have the "costraint forces" data to plot my results. But, in SOL 600 I am not able...
Dear all,
I am using SOL 600 implicit nonlinear solver to simulate the progressive failure analysis of a multilayered composite laminate. And I used Puck failure criteria while defining material properties with gradual failure option selected. I am simulating the progressive failure analysis of...