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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: 266
Whey-Pone Tsai , Nat. Center for High Performance Comput., Hsin-Chu, Taiwan
Yang-Yao Niu , Nat. Center for High Performance Comput., Hsin-Chu, Taiwan
ABSTRACT
A dual time-step integration method with a preconditioned upwind scheme for the simulation of low Mach number flow is applied to an aerodynamic analysis of high-lift airfoils. Third-order flux extrapolation in conjunction with Roe's (1981) flux splitting is chosen for spatial discretization. An implicit real-time discretization is used and the governing equations are evaluated by a two-stage Runge-Kutta scheme, while converged solutions are calculated in each pseudo-time-step. Also, local time stepping and residual smoothing methods are implemented to accelerate convergence. Aerodynamic loading of high-lift systems, including an oscillating NACA0012 airfoil and a NACA4412 airfoil with a Gurney flap, are simulated in this study. The simulated results show that the numerical predictions agree with the validated computed results or experimental data. The performance statistics of parallelization and vectorization on Cray and Fujitsu vector machines for the current study are also investigated.
INDEX TERMS
aerodynamics; aerodynamic analysis; high-lift airfoils; dual time-step integration method; upwind splitting; preconditioned upwind scheme; low Mach number flow; 3rd-order flux extrapolation; flux splitting; spatial discretization; implicit real-time discretization; governing equations; two-stage Runge-Kutta scheme; converged solutions; local time stepping; residual smoothing methods; convergence acceleration; aerodynamic loading; oscillating NACA0012 airfoil; NACA4412 airfoil; Gurney flap; simulation; Cray computer; Fujitsu computer; vector machines; performance statistics; parallelization; vectorization
CITATION
Whey-Pone Tsai, Yang-Yao Niu, "Aerodynamic analysis of high-lift airfoils by a dual-time integration method with upwind splitting", High Performance Computing and Grid in Asia Pacific Region, International Conference on, vol. 00, no. , pp. 266, 1997, doi:10.1109/HPC.1997.592158
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