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Boundary ConditionsHello ,
I am writing a Finite Volume method code for isentropic flow through a converging diverging nozzle . I am modelling half of the nozzle due to symmetry about the center line .I am not sure how to apply the Symmetry Boundary Condition .Here is the code I have written for the Symmetry Boundary Condition and the Wall Boundary Condition . Can someone please tell me if it is correct ? u represents the horizontal velocity through the nozzle ;v the vertical component of velocity ;a is the speed of sound ;d -density ; e- internal energy . the profile of the nozzle is taken as y=0.5 +1.1(x-1.5)^2 ; for(i=1;i<=210;i++) { k=120; p[i][k+1]=p[i][k]; theta = atan(2.2*(x[i][k]-1.5)); //The above line calculates the tangential direction along the upper wall of nozzle// if(theta>=0){ u[i][k+1]=u[i][k]*cos(2.0*theta) + v[i][k]*sin(2.0*theta) ; v[i][k+1]=u[i][k]*sin(2.0*theta) - v[i][k]*cos(2.0*theta); } else { v[i][k+1] =-(u[i][k]*sin(-2.0*theta) + v[i][k]*cos(-2.0*theta)); u[i][k+1] = u[i][k]*cos(-2.0*theta)- v[i][k]*sin(-2.0*theta); } a[i][k+1]=a[i][k]; d[i][k+1]=d[i][k]; e[i][k+1]=e[i][k]; } Symmetry Boundary Condition ; for(i=1;i<=nx;i++) { pb[i]=p[i][1]; ub[i]=u[i][1]; vb[i]=0.0; ab[i]=a[i][1]; db[i]=d[i][1]; eb[i]=e[i][1]; } Waiting eagerly for some help. Regards . Victor . |

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