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<RAE "A" 날개-축대칭 동체> 비행체 형상에 대한 천음속 점성 유동의 수치적 연구
임예훈(Y.H. Im),장근식(K.S. Chang),정희권(H.K. Jeong),권장혁(J.H. Kwon),박민우(M.W. Park) 한국전산유체공학회 1997 한국전산유체공학회 학술대회논문집 Vol.1997 No.-
The Computer code KAIST-ADD LUFUNS has been developed to solve 3D compressible turbluent flow. This method employs Harten-Yee's modified upwind scheme in the explicit part and Steger-Warming Splitting in the implicit part. Flow past RAE wing-body aircraft has been computed for three different flow conditions. The results have shown good comparision with the experimental data. Baldwin-Lomax turbluence model is used for this computer code.
Chimera 격자계를 이용한 Euler/Navier-Stokes Solver의 개발
이승수(S. Lee),박민우(M. Park),조금원(K. W. Cho),권장혁(J. H. Kwon) 한국전산유체공학회 1998 한국전산유체공학회 학술대회논문집 Vol.1998 No.-
An Euler/Navier Stokes solver has been developed for the analysis of steady and unsteady flows. The q-ω turbulent model has been incorporated into the solver in strongly coupled manner for stability and robustness. A new Chimera hole cutting algorithm, Cut-paste algorithm, has been devised for automatic Chimera hole cutting. Number of viscous/inviscid numerical computations demonstrate the accuracy and the versatility of the solver.