📄 soli8s.m
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function [es,et,eci]=soli8s(ex,ey,ez,ep,D,ed)
% [es,et,eci]=soli8s(ex,ey,ez,ep,D,ed)
%-------------------------------------------------------------
% PURPOSE
% Calculate element normal and shear stress for a
% 8 node (brick) isoparametric element.
%
% INPUT: ex = [x1 x2 x3 ... x8]
% ey = [y1 y2 y3 ... y8] element coordinates
% ez = [z1 z2 z3 ... z8]
%
% ep = [Ir] Ir: integration rule
%
% D constitutive matrix
%
% ed = [u1 u2 ..u24; element displacement vector
% ...........] one row for each element
%
% OUTPUT: es = [ sigx sigy sigz sigxy sigyz sigxz ;
% ...... ... ]
% element stress matrix, one row for each element
%-------------------------------------------------------------
% LAST MODIFIED: M Ristinmaa 1995-10-25
% Copyright (c) Division of Structural Mechanics and
% Department of Solid Mechanics.
% Lund Institute of Technology
%-------------------------------------------------------------
ir=ep(1); ngp=ir*ir*ir;
%--------- gauss points --------------------------------------
if ir==2
g1=0.577350269189626; w1=1;
gp(:,1)=[-1; 1; 1;-1;-1; 1; 1;-1]*g1; w(:,1)=[ 1; 1; 1; 1; 1; 1; 1; 1]*w1;
gp(:,2)=[-1;-1; 1; 1;-1;-1; 1; 1]*g1; w(:,2)=[ 1; 1; 1; 1; 1; 1; 1; 1]*w1;
gp(:,3)=[-1;-1;-1;-1; 1; 1; 1; 1]*g1; w(:,3)=[ 1; 1; 1; 1; 1; 1; 1; 1]*w1;
elseif ir==3
g1=0.774596669241483; g2=0.;
w1=0.555555555555555; w2=0.888888888888888;
I1=[-1; 0; 1;-1; 0; 1;-1; 0; 1]'; I2=[ 0;-1; 0; 0; 1; 0; 0; 1; 0]';
gp(:,1)=[I1 I1 I1]'*g1; gp(:,1)=[I2 I2 I2]'*g2+gp(:,1);
I1=abs(I1); I2=abs(I2);
w(:,1)=[I1 I1 I1]'*w1; w(:,1)=[I2 I2 I2]'*w2+w(:,1);
I1=[-1;-1;-1; 0; 0; 0; 1; 1; 1]'; I2=[ 0; 0; 0; 1; 1; 1; 0; 0; 0]';
gp(:,2)=[I1 I1 I1]'*g1; gp(:,2)=[I2 I2 I2]'*g2+gp(:,2);
I1=abs(I1); I2=abs(I2);
w(:,2)=[I1 I1 I1]'*w1; w(:,2)=[I2 I2 I2]'*w2+w(:,2);
I1=[-1;-1;-1;-1;-1;-1;-1;-1;-1]'; I2=[ 0; 0; 0; 0; 0; 0; 0; 0; 0]';
I3=abs(I1);
gp(:,3)=[I1 I2 I3]'*g1; gp(:,3)=[I2 I3 I2]'*g2+gp(:,3);
w(:,3)=[I3 I2 I3]'*w1; w(:,3)=[I2 I3 I2]'*w2+w(:,3);
else
disp('Used number of integration points not implemented');
return
end
wp=w(:,1).*w(:,2).*w(:,3);
xsi=gp(:,1); eta=gp(:,2); zet=gp(:,3); r2=ngp*3;
%--------- shape functions -----------------------------------
N(:,1)=(1-xsi).*(1-eta).*(1-zet)/8; N(:,5)=(1-xsi).*(1-eta).*(1+zet)/8;
N(:,2)=(1+xsi).*(1-eta).*(1-zet)/8; N(:,6)=(1+xsi).*(1-eta).*(1+zet)/8;
N(:,3)=(1+xsi).*(1+eta).*(1-zet)/8; N(:,7)=(1+xsi).*(1+eta).*(1+zet)/8;
N(:,4)=(1-xsi).*(1+eta).*(1-zet)/8; N(:,8)=(1-xsi).*(1+eta).*(1+zet)/8;
dNr(1:3:r2,1)=-(1-eta).*(1-zet); dNr(1:3:r2,2)= (1-eta).*(1-zet);
dNr(1:3:r2,3)= (1+eta).*(1-zet); dNr(1:3:r2,4)=-(1+eta).*(1-zet);
dNr(1:3:r2,5)=-(1-eta).*(1+zet); dNr(1:3:r2,6)= (1-eta).*(1+zet);
dNr(1:3:r2,7)= (1+eta).*(1+zet); dNr(1:3:r2,8)=-(1+eta).*(1+zet);
dNr(2:3:r2+1,1)=-(1-xsi).*(1-zet); dNr(2:3:r2+1,2)=-(1+xsi).*(1-zet);
dNr(2:3:r2+1,3)= (1+xsi).*(1-zet); dNr(2:3:r2+1,4)= (1-xsi).*(1-zet);
dNr(2:3:r2+1,5)=-(1-xsi).*(1+zet); dNr(2:3:r2+1,6)=-(1+xsi).*(1+zet);
dNr(2:3:r2+1,7)= (1+xsi).*(1+zet); dNr(2:3:r2+1,8)= (1-xsi).*(1+zet);
dNr(3:3:r2+2,1)=-(1-xsi).*(1-eta); dNr(3:3:r2+2,2)=-(1+xsi).*(1-eta);
dNr(3:3:r2+2,3)=-(1+xsi).*(1+eta); dNr(3:3:r2+2,4)=-(1-xsi).*(1+eta);
dNr(3:3:r2+2,5)= (1-xsi).*(1-eta); dNr(3:3:r2+2,6)= (1+xsi).*(1-eta);
dNr(3:3:r2+2,7)= (1+xsi).*(1+eta); dNr(3:3:r2+2,8)= (1-xsi).*(1+eta);
dNr=dNr/8.;
%--------- three dimensional case ----------------------------
rowed=size(ed,1);
rowex=size(ex,1);
if rowex==1 incie=0; else incie=1; end
es=[]; et=[]; eci=[]; ie=1;
for ied=1:rowed
eci=[eci N*[ex(ie,:);ey(ie,:);ez(ie,:)]'];
JT=dNr*[ex(ie,:);ey(ie,:);ez(ie,:)]';
for i=1:ngp
indx=[ 3*i-2; 3*i-1; 3*i ];
detJ=det(JT(indx,:));
if detJ<10*eps
disp('Jacobideterminant equal or less than zero!')
end
JTinv=inv(JT(indx,:));
dNx=JTinv*dNr(indx,:);
B(1,1:3:24-2)=dNx(1,:);
B(2,2:3:24-1)=dNx(2,:);
B(3,3:3:24) =dNx(3,:);
B(4,1:3:24-2)=dNx(2,:);
B(4,2:3:24-1)=dNx(1,:);
B(5,1:3:24-2)=dNx(3,:);
B(5,3:3:24) =dNx(1,:);
B(6,2:3:24-1)=dNx(3,:);
B(6,3:3:24) =dNx(2,:);
ee=B*ed(ied,:)';
et=[et; ee'];
es=[es; (D*ee)'];
end
ie=ie+incie;
end
%--------------------------end--------------------------------
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