📄 shelltr.h
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#ifndef SHELLTR_H#define SHELLTR_H#include "alias.h"struct matrix;struct vector;struct ivector;/** shell triangular element resulting matrices are composed from plane triangular element with rotational degrees of freedom and from constant curve triangle */class shelltr{ public: shelltr (void); ~shelltr (void); void eleminit (long eid); void tran_mat(vector &x, vector &y, matrix &tran, vector &gx, vector &gy, vector &gz); void transf_matrix (ivector &nodes,matrix &tmat); void res_stiffness_matrix (long eid,matrix &sm); void appval (vector &l,vector &eps,double **val); void res_mainip_strains (long lcid,long eid); void nod_strains (long lcid,long eid); void elem_strains (double **stra,long lcid,long eid); void appstrain (long lcid,long eid,vector &l,vector &eps); void allip_strains (double **stra,long lcid,long eid); void strains (long lcid,long eid); void res_mainip_stresses (long lcid,long eid); void nod_stresses (long lcid,long eid); void elem_stresses (double **stra,double **stre,long lcid,long eid); void appstress (long lcid,long eid,vector &l,vector &eps); void allip_stresses (double **stre,long lcid,long eid); void stresses (long lcid,long eid); void inicipval(long eid, long ri, long ci, matrix &nodval, inictype *ictn); // number of DOFs on the element long ndofe; // number of nodes on one element long nne; // number of edges on one element long ned; // number of nodes on one edge long nned; /// total number of integration points on element long tnip; // order of integration of stiffness matrix long **intordsm; // total number of components of stress and strain tensors long tncomp,tncomps,tncompd; // number of components of stress and strain tensors plane long *ncomps; // number of components of stress and strain tensors plate long *ncompd; // number of approximated functions on the element long napfun; // array of numbers of DOFs long *dofe; // number of integration points for stiffness matrix long **nip; // number of blocks long nb; // stress/strain state strastrestate ssst; };#endif
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