1. Computation of a transonic finite wing flow using Hanbit-1 computer
- Author
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Moon-Gyu Kim, S.O. Park, and S.M. Cho
- Subjects
Runge–Kutta methods ,Flow (mathematics) ,Computer science ,Iterative method ,Computation ,MathematicsofComputing_NUMERICALANALYSIS ,Domain decomposition methods ,Aerodynamics ,Hypercube ,Transonic ,Computational science - Abstract
This paper reports the results of a parallel computation of a transonic flow past a 3D wing using the Hanbit-1 computer, a hypercube parallel computer developed at KAIST (Korea Advanced Institute of Science and Technology). Two different numerical schemes, one a lower-upper symmetric Gauss-Seidel (LU-SGS) method and the other a Runge-Kutta time-stepping scheme, were used. The performance of the Hanbit-1 was assessed based on the present parallel computation with domain decomposition.
- Published
- 2002
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