The Community for Technology Leaders
High Performance Computing and Grid in Asia Pacific Region, International Conference on (1997)
Seoul, Korea
Apr. 28, 1997 to May 2, 1997
ISBN: 0-8186-7901-8
pp: 85
S.M. Cho , Dept. of Aerosp. Eng., Korea Adv. Inst. of Sci. & Technol., Seoul, South Korea
M.H. Kim , Dept. of Aerosp. Eng., Korea Adv. Inst. of Sci. & Technol., Seoul, South Korea
S.O. Park , Dept. of Aerosp. Eng., Korea Adv. Inst. of Sci. & Technol., Seoul, South Korea
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.
INDEX TERMS
transonic flow; transonic finite wing flow; Hanbit-1 computer; parallel computation; 3D wing; hypercube parallel computer; numerical schemes; lower-upper symmetric Gauss-Seidel method; Runge-Kutta time-stepping scheme; performance assessment; domain decomposition
CITATION
S.M. Cho, M.H. Kim, S.O. Park, "Computation of a transonic finite wing flow using Hanbit-1 computer", High Performance Computing and Grid in Asia Pacific Region, International Conference on, vol. 00, no. , pp. 85, 1997, doi:10.1109/HPC.1997.592127
81 ms
(Ver 3.3 (11022016))