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Extra resources for FINITE ELEMENT METHOD PROGRAMMING WITH MATHEMATICA - AIRPLANE DESIGN
Sample text
C symb {E, nu, alpha, rho} building a MCPT with several materials. The table is then printed with the module PrintMasterConstitutivePropertyTable described below. 2. 3, retrieves the cPL of an individual material given the code number. The arguments are the MCPT and ccod, and the function returns the appropriate cPL if the material exists. Note that in the case of a built-in material, access is by its negative code number . This assumes that a mapping from the material name to its code has been effected.
If the plate or shell is still homogeneous but orthotropic, orientation data is required. As a fairly complex example consider a laminated plate built up of 8 layers of orthotropic composite materials. 2. The 8 layer thicknesses must be stored as fabrication extent properties. And 8 sets of material directions data (which in most practical cases would consist of one rotation angle) must be stored as fabrication orientation data. 1. Principal material directions {xm , ym , z m } for a orthothropic solid element.
We are now ready to introduce the Individual Fabrication Property List or fPL. There is one fPL for each defined geometric property code. 1) The first two items are keywords. Fabrication-id steers the processing and interpretation of the 6–3 Chapter 6: ELEMENT FABRICATION PROPERTIES 6–4 property value list, and can provide valuable crosschecks against element definition data. Plate" may be used to indicate that the property table is for an isotropic homogeneous C 1 plate element, whereas "MFC" identifies properties appropriate to a MultiFreedom Constraint element.