TURBULENT FLOW SIMULATIONS ABOUT THE AIRCRAFT CONFIGURATION항공기 주위 난류 유동자아 해석

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 393
  • Download : 1193
An 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.
Publisher
한국전산유체공학회
Issue Date
2005-12
Keywords

Turbulent Flow Simulation; Multigrid; k-ω WD+ Turbulent model; Drag Prediction; Grid Convergence Study; Turbulent Flow Simulation; Multigrid; k-ω WD+ Turbulent model; Drag Prediction; Grid Convergence Study

Citation

한국전산유체공학회지, Vol.10, No.4, pp.39-50

URI
http://hdl.handle.net/10203/9608
Link
http://www.kscfe.or.kr/
Appears in Collection
AE-Journal Papers(저널논문)
Files in This Item
dbpia0684201.pdf(4.87 MB)Download

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0