A multilevel composite grid method for fluid flow computations

Author:

SHYY W.1,WRIGHT J.1,LIU J.1

Affiliation:

1. Florida Univ., Gainesville

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. 3078,P. 1-10. computation. Fora Reynolds number of 106,with-the multigrid solution procedure described above, the speed-up ratio, in terms of total workunit ratio,obtained fortwomultigrid levels is 2.37,andthatobtainedusingall three multigrid levels is 3.39. For a Reynolds number of 800thecorrespondingspeed-upsare 1.28and 1.72.Figure 16showsacomparisonbetweentheconvergencepathsof the single-level and multi-level computations for both Reynolds numbers. The speed-up ratios obtained for this configurationshowsthatevenforverycomplexcomposite grid configurations, the multigrid efficiency is largely maintained even with the use of composite gridding. In general, for any composite grid configuration, the maximum attainable speed-up ratio will be determined roughly by the smallest grid block of the composite grid system. For the baffleflow, the smallestgrid block has a resolution of 21x53 nodes (blocks one and seven), therefore, one would expect the speed-up ratio to fall

2. On the use of composite grid schemes in computational aerodynamics

3. Composite overlapping meshes for the solution of partial differential equations

4. A composite grid approach for the Euler equations

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. SEQUENTIAL PRESSURE-BASED NAVIER-STOKES ALGORITHMS ON SIMD COMPUTERS: COMPUTATIONAL ISSUES;Numerical Heat Transfer, Part B: Fundamentals;1994-09

2. REFERENCES;Computational Modeling for Fluid Flow and Interfacial Transport;1994

3. Elements of Pressure-Based Computational Algorithms for Complex Fluid Flow and Heat Transfer;Advances in Heat Transfer Volume 24;1994

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