Computational Fluid Dynamics is the Future

Computational Fluid Dynamics is the Future MAIN PAGE MATLAB

RESEARCH CFD MODELLING

GAS/STEAM TURBINES ESI SOFTWARE SUBMARINES

EXPERIMENTATION FOR CFD AERODYNAMICS

FORTRAN90

OPENFOAM

CAE ( FINITE ELEMENT OPEN SOURCE) CO2 MEASURMENTS

TRNSYS

ANSYS-CFX

AIRCRAFT DESIGN REAL FLOW

ANSYS FLUENT

GEOMETRICAL MODELLING SOFTWARE CHEMKIN

NUMECA FINE/TURBO SALOME-PLATFORM

ANSYS STRESS ANALYSIS

CHEMICAL WORKBENCH

PYTHON FLASH

BOX2D

NX CAE

STAR-CCM+

SPACE RACE C++

TECPLOT

MACHINE DESIGN

XM GRACE

MICRO TURBINE

Putting Togather the Right hand Side of the Navier Stokes Equation   clc  clear  L=30;  M=30;  N=30;  time=10;  for t=1:time;  for i=1:L;  for j=1:M;  for k=1:N;  u(i,j,k,t)=randn(1,1);  v(i,j,k,t)=randn(1,1);  w(i,j,k,t)=randn(1,1);  dudx(i,j,k,t)=randn(1,1);  dudy(i,j,k,t)=randn(1,1);  dudz(i,j,k,t)=randn(1,1);  RS(i,j,k,t)=u(i,j,k,t)*dudx(i,j,k,t)+v(i,j,k,t)*dudy(i,j,k,t)+w(i,j,k,t)*dudz(i,j,k,t);  end  end 

end  end  figure('Position',[5 5 1700 900])  contour(RS(:,:,1,3),12)  xlabel('x axis')  ylabel('y axis')  title('Plotting the Right Hand Side')  set(gca,'XLim',[0 M],'YLim',[0 N])  grid on

Navier Stokes Equations  %Navire_stokes  %u  %v  %w  %du/dx  %du/dy  %du/dz  %d2u/dx2  %mu  clc  clear  N=5;  M=5;  mu=1.2*0.00001;  delta_t=0.001;  dx=0.01;  dy=0.01;  dz=0.01;  n=0;  nn=0;  for t=1:10;      n=n+1;      if (t==1)          t=n;  for i=1:N;      for j=1:M;          u(i,j,t)=randn(1,1);          v(i,j,t)=randn(1,1);          w(i,j,t)=randn(1,1);          dudx(i,j,t)=randn(1,1);          dudy(i,j,t)=randn(1,1);          dudz(i,j,t)=randn(1,1);          d2udx2(i,j,t)=randn(1,1);          dvdx(i,j,t)=randn(1,1);          dvdy(i,j,t)=randn(1,1);          dvdz(i,j,t)=randn(1,1);          d2vdx2(i,j,t)=randn(1,1); 

        dpdx(i,j,t)=1.3/dx;          dpdy(i,j,t)=3.2/dy;      end  end  for i=1:N;      for j=1:M;          RHS1(i,j,t)=­u(i,j,t)*dudx(i,j,t)­v(i,j,t)*dudy(i,j,t)­w(i,j,t)*dudz(i,j,t)+mu*d2udx2(i,j,t)­dpdx(i,j,t);          RHS2(i,j,t)=­u(i,j,t)*dvdx(i,j,t)­v(i,j,t)*dvdy(i,j,t)­w(i,j,t)*dvdz(i,j,t)+mu*d2vdx2(i,j,t)­dpdy(i,j,t);          RHS3(i,j,t)=randn(1,1);      end  end  for i=1:N;      for j=1:M;      u(i,j,t+1)=u(i,j,t)+delta_t*RHS1(i,j,t);      v(i,j,t+1)=v(i,j,t)+delta_t*RHS2(i,j,t);      w(i,j,t+1)=w(i,j,t)+delta_t*RHS3(i,j,t);      total=[ u(i,j,t+1) v(i,j,t+1) w(i,j,t+1)];      v(i,j,t)=norm(total);      end  end  elseif (t>1)  nn=nn+1;  t=nn;  for i=1:N;      for j=1:M;          dudx(i,j,t)=u(i,j,t)/dx;          dudy(i,j,t)=u(i,j,t)/dy;          dudz(i,j,t)=u(i,j,t)/dz;          d2udx2(i,j,t)=u(i,j,t)/(dx*dx);          dvdx(i,j,t)=v(i,j,t)/dx;          dvdy(i,j,t)=v(i,j,t)/dy;          dvdz(i,j,t)=v(i,j,t)/dz;         d2vdx2(i,j,t)=v(i,j,t)/(dx*dx);          dpdx(i,j,t)=1.3/dx;          dpdy(i,j,t)=3.2/dy;          RHS1(i,j,t)=­u(i,j,t)*dudx(i,j,t)­v(i,j,t)*dudy(i,j,t)­w(i,j,t)*dudz(i,j,t)+mu*d2udx2(i,j,t)­dpdx(i,j,t);          RHS2(i,j,t)=­u(i,j,t)*dvdx(i,j,t)­v(i,j,t)*dvdy(i,j,t)­w(i,j,t)*dvdz(i,j,t)+mu*d2vdx2(i,j,t)­dpdy(i,j,t);          RHS3(i,j,t)=randn(1,1);      end  end  for i=1:N;      for j=1:M;      u(i,j,t+1)=u(i,j,t)+delta_t*RHS1(i,j,t);      v(i,j,t+1)=v(i,j,t)+delta_t*RHS2(i,j,t);      w(i,j,t+1)=w(i,j,t)+delta_t*RHS3(i,j,t);      total=[ u(i,j,t+1) v(i,j,t+1) w(i,j,t+1)]; 

    v(i,j,t)=norm(total);      end  end      end  end

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