📄 aco2i4d.m
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function [Ke,Me,fe]=aco2i4d(ex,ey,ep,eq)% [Ke,Me]=aco2i4d(ex,ey,ep)% [Ke,Me,fe]=aco2i4d(ex,ey,ep,eq)%-------------------------------------------------------------% PURPOSE% Compute element stiffness and mass % matrix for 4 node isoparametric acoustic element%% INPUT: ex = [x1 x2 x3 x4] element coordinates% ey = [y1 y2 y3 y4]% % ep = [t c raa ir] thickness, speed of sound, % density, integration rule%% eq mass inflow per unit volume% and time (second derivative)%% OUTPUT: Ke : element 'stiffness' matrix (4 x 4)% Me : element mass matrix (4 x 4)% fe : element load vector (4 x 1)%-------------------------------------------------------------% LAST MODIFIED: G Sandberg 1996-03-08% Copyright (c) Division of Structural Mechanics and% Department of Solid Mechanics.% Lund Institute of Technology%------------------------------------------------------------- t=ep(1); c=ep(2); raa=ep(3); ir=ep(4); ngp=ir*ir; if nargin==3; eq=0 ; end if ir==1 g1=0.0; w1=2.0; gp=[ g1 g1 ]; w=[ w1 w1 ]; elseif ir==2 g1=0.577350269189626; w1=1; gp(:,1)=[-g1; g1;-g1; g1]; gp(:,2)=[-g1;-g1; g1; g1]; w(:,1)=[ w1; w1; w1; w1]; w(:,2)=[ w1; w1; w1; w1]; elseif ir==3 g1=0.774596699241483; g2=0.; w1=0.555555555555555; w2=0.888888888888888; gp(:,1)=[-g1;-g2; g1;-g1; g2; g1;-g1; g2; g1]; gp(:,2)=[-g1;-g1;-g1; g2; g2; g2; g1; g1; g1]; w(:,1)=[ w1; w2; w1; w1; w2; w1; w1; w2; w1]; w(:,2)=[ w1; w1; w1; w2; w2; w2; w1; w1; w1]; else disp('Used number of integration points not implemented'); return end wp=w(:,1).*w(:,2); xsi=gp(:,1); eta=gp(:,2); r2=ngp*2; N(:,1)=(1-xsi).*(1-eta)/4; N(:,2)=(1+xsi).*(1-eta)/4; N(:,3)=(1+xsi).*(1+eta)/4; N(:,4)=(1-xsi).*(1+eta)/4; dNr(1:2:r2,1)=-(1-eta)/4; dNr(1:2:r2,2)= (1-eta)/4; dNr(1:2:r2,3)= (1+eta)/4; dNr(1:2:r2,4)=-(1+eta)/4; dNr(2:2:r2+1,1)=-(1-xsi)/4; dNr(2:2:r2+1,2)=-(1+xsi)/4; dNr(2:2:r2+1,3)= (1+xsi)/4; dNr(2:2:r2+1,4)= (1-xsi)/4; Ke1=zeros(4,4); Me1=zeros(4,4); fe1=zeros(4,1); JT=dNr*[ex;ey]'; for i=1:ngp indx=[ 2*i-1; 2*i ]; detJ=det(JT(indx,:)); if detJ<10*eps disp('Jacobideterminanten lika med noll!') end JTinv=inv(JT(indx,:)); B=JTinv*dNr(indx,:); Ke1=Ke1+B'*B*detJ*wp(i); Me1=Me1+N(i,:)'*N(i,:)*detJ*wp(i); fe1=fe1+N(i,:)'*detJ*wp(i); end Ke=Ke1*t*c*c; Me=Me1*t; fe=fe1*t*c*c*raa*eq;%--------------------------end--------------------------------
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