📄 soli8f.m
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function [ef]=soli8e(ex,ey,ez,ep,es)% ef=soli8f(ex,ey,ez,ep,es)%-------------------------------------------------------------% PURPOSE% Calculate the element force vector 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%% es element stress matrix% bz: body force in z direction%% OUTPUT: ef=[f1 f2 ...f24]%-------------------------------------------------------------% 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 ---------------------------- [rowes,colD]=size(es); rowex=size(ex,1); if rowex==1 incie=0; else incie=1; end ef=[]; ir=0; ie=1; for ied=1:rowes/ngp JT=dNr*[ex(ie,:);ey(ie,:);ez(ie,:)]'; indx=[1:3]'; fint=zeros(24,1); for i=1:ngp ir=ir+1; 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,:); fint=fint+B'*es(ir,:)'*wp(i)*detJ; indx=indx+3; end ef=[ef; fint']; ie=ie+incie; end%--------------------------end--------------------------------
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