$$$$ @LAFAIL NOTICE CHAT 11/09/12 21:16:50 7124 DATE 11/09/12 Procedure @LAFAIL Voir aussi : @LAREAD ----------------- @LAFAIL TAB_LAM TAB_FAIL ; Description : ------------- This procedure makes it possible to check the ultimate breaking-strength of a multilayer by setting to zero the elastic properties of the plies on the point of breaking. with TAB_LAM Characteristics table of the multilayer TAB_FAIL Characteristic table for carrying out a multilayer breaking-strength calculation The table contains on input : Index Description 'SOUSTYPE' MOT of 'LAMINATE_FAIL' value 'TYP_FAIL' MOT for identifying the type of checking to be performed It can be : 'FPF' : First Ply Failure (Default) 'LPF' : Last Ply Failure 'ITERMAX' maximum ENTIER number of iterations for convergence (Default 10) 'PREC' FLOTTANT indicates the convergence precision value (Default 1.e-2) 'CLIM' RIGIDITE object of the boundary conditions 'CHARG' CHPOINT object of the loading 'RIG2' RIGIDITE object for an additional stiffness in addition to the multilayer (Optional) and on output : 'FMF' Loading multiplying factor for the First Ply Failure 'NPF' Index of the First Ply Failure 'NZF' Index of the region to which the First Ply Failure pertains 'FML' Loading multiplying factor for the Last Ply Failure
© Cast3M 2003 - All rights reserved.
Disclaimer