By Edward Sang
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Extra resources for A new table of seven-place logarithms
To reduce computational cost it is carried out on the first free surface timestep of each baroclinic one. [. l LJ,'--LJ" -- 4- 2- 0 i 0 , l I I 500 i i , , I i 1000 i J i I ' 1500 i , l I 2000 i i , , I 2500 i i , i I 3000 i i i i I 3500 Timestep no. Figure 2: Number of seconds spent in each call to subroutine step for a 256 processor run.
Biederman, B. , Gleixner, A. J. and Yetka, C. , "Development and Application of a Multistage Navier-Stokes Solver, Part II: Application to a High Pressure Compressor Design," presented at The 40th ASME Gas Turbine Conference, Houston, Texas, June 5-8, 1995. Parallel ComputationalFluid Dynamics: Implementations and Results Using Parallel Computers A. Ecer, J. Periaux, N. Satofuka and S. V. All rights reserved. N, URA 740, University Claude Bernard Lyon 1, Bat101, 43 Bd du 11 Novembre 1918, 69622 Villeurbanne cedex, France In this paper we study the computation of combustion fronts using MIMD architecture with up to 200 nodes.
Let us describe briefly the method. We consider first the example of a scalar equation: 0-7 = Oz-Z + o, with some appropriate initial condition. We suppose that u exhibits a TL of e thickness located at z = S(t) E (-1,1) and we suppose that S is such that F~(u(z,t)) reaches its maximum at z = S(t), with F~ = O(1). We recall the properties of pseudospectral approximations with Chebyshev polynomials on a single domain of computation denoted ~2 and with no adaptivity. Let fl be a compact subset of the interval [-1,1] and u E C~(ft).
A new table of seven-place logarithms by Edward Sang