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hello in a previous video we discussed how to create and edit global plies and in this video we discuss how to post-process laminate results which make use of global plies in this model we have a composite fitting the blue elements are made up of a six ply layup and the purple elements are made up of as ten ply layout we already have results analysis results for sixteen different load cases but before we look at any of the results letamp;#39;s first review our layups the ten ply layup is an alternating 45 0 45 pattern that is a symmetric 10 ply laminate of a plain weave carbon fabric material is defined by global plies 1 through global ply 10 the 6 ply layup itamp;#39;s the same pattern but simply global plies 3 through 8 now letamp;#39;s toggle to post-processing change the contour style to contour we will leave the output set on load case 1 I mean change the vector that weamp;#39;re plotting to laminate apply 1 X normal stress when we look at the X normal stress itamp;#39;s impo
