TURBULENT FLOW SIMULATIONS ABOUT THE AIRCRAFT CONFIGURATION항공기 주위 난류 유동자아 해석

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dc.contributor.authorKim, Yoonsik-
dc.contributor.authorPark, Soo Hyung-
dc.contributor.authorKwon, Jang-Hyuk-
dc.contributor.author김, 윤식-
dc.contributor.author박, 수형-
dc.contributor.author권, 장혁-
dc.date.accessioned2009-06-18T08:28:04Z-
dc.date.available2009-06-18T08:28:04Z-
dc.date.issued2005-12-
dc.identifier.citation한국전산유체공학회지, Vol.10, No.4, pp.39-50en
dc.identifier.urihttp://www.kscfe.or.kr/-
dc.identifier.urihttp://hdl.handle.net/10203/9608-
dc.description.abstractAn application of the KFLOW3D code which has been developed at KAIST is presented. This paper briefly describes the underlying methodology and summarizes the results for the DLR-F6 transport configuration recently presented in the second AIAA CFD Drag Prediction Workshop held in Orlando, FL, June 2003. KFLOW3D is a parallelized Reynolds averaged Navier-Stokes solver for multi-block structured grids. For the present computations, 2-equation k-ω WD+ nonlinear eddy viscosity model is used. The emphasis of the paper is placed on the implementation of the k-ω WD+ model in the multigrid framework and practicality of KFLOW3D for accurately predicting not only the integrated aerodynamic property such as the drag coefficient but pressure distributions.en
dc.description.sponsorshippartially supported by the "Dual Use Technology Program" of the MOCIEen
dc.language.isoen_USen
dc.publisher한국전산유체공학회en
dc.subjectTurbulent Flow Simulation-
dc.subjectMultigrid-
dc.subjectk-ω WD+ Turbulent model-
dc.subjectDrag Prediction-
dc.subjectGrid Convergence Study-
dc.subjectTurbulent Flow Simulation-
dc.subjectMultigrid-
dc.subjectk-ω WD+ Turbulent model-
dc.subjectDrag Prediction-
dc.subjectGrid Convergence Study-
dc.titleTURBULENT FLOW SIMULATIONS ABOUT THE AIRCRAFT CONFIGURATIONen
dc.title.alternative항공기 주위 난류 유동자아 해석en
dc.typeArticleen
dc.language.Alternativekoen

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