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Abstracts - KTH Mechanics

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55<br />

Development of a 3D transient incompressible Navier-Stokes solver<br />

N. Suresh Kumar a, Anoop K. Dass a and Manmohan Pandey a<br />

This work is concerned with the development of a 3D transient Navier-Stokes solver<br />

through finite difference method. The solver is based on the fractional step method<br />

proposed by Choi and Moin 1. The spatial discretization of the convective fluxes is carried<br />

out through Kuwahara’s third order upwind scheme 2 and viscous fluxes through a fourth<br />

order central difference scheme. In the fractional step method of Choi and Moin 1, every<br />

time step is advanced in four substeps. The method requires the solution of pressure<br />

Poisson equation in only one substep. In this method, continuity equation is satisfied only<br />

at the final substep. In the present code, the pressure Poisson equation is solved through a<br />

multigrid procedure with flexibility in choosing the number of levels to accelerate<br />

convergence. As the code is third order accurate in space and second order accurate in time,<br />

and multigrid accelerates its rate of convergence, it has DNS potential. However, the results<br />

presented here are for the steady state laminar flow in a 3D cubical cavity for Re=1000 on a<br />

129129129 staggered grid, which have been obtained through the code in a timemarching<br />

fashion. Figure 1(a) shows the projection of streamlines on the cavity mid-plane<br />

and Figure 1(b) compares the centreline x-velocity with those of Renwei et al. 3 and 2D<br />

results produced on a 129129 grid. Our results compare well with those of Ref. 3 and<br />

deviate from the 2D results, as expected.<br />

a<br />

Indian Institute of Technology Guwahati, Guwahati 781039, India<br />

1<br />

Choi and Moin, J. Comp. Physics, 113, 1 (1994)<br />

2<br />

Kawamura and Kuwahara, AIAA-85-0376 (1985)<br />

3<br />

Renwei et al., J. Comp. Physics, 161, 680 (2000)<br />

(a)<br />

Figure 1: (a) Projection of streamlines on the mid-plane, (b) Comparison of centreline xvelocity,<br />

for Re=1000<br />

(b)

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