Forschung im HLRN-Verbund 2011

155c lc dc lc dα cαFigure 1: Lift polar (top) and contour plot of pressure coefficient with stream traces based on skin-friction (bottom).More Information1. KROLL, N., ROSSOW, C.-C., SCHWAM-BORN, D., BECKER, K. AND HELLER, G:MEGAFLOW - A Numerical Flow SimulatonTool for Transport Aircraft Design. ICASCongress 2002, Toronto, 09.-13.09.2002, ICAS2. SCHWAMBORN, D., GERHOLD, T., ANDHEINRICH ,R.: The DLR TAU-Code: Recentapplications in Research and Industry. In: P.Wesseling, E. Oate, J. Priaux (Eds), ECCOMASCFD, Egmond aan Zee, The Netherlands, 20063. http://www.centaursoft.com/4. MENTER, F. R.: Zonal two-equation k-ω turbulencemodels for aerodynamic flows. In: AIAAPaper, AIAA - 93 -2906 (1993)5. GROTE, A. AND RADESPIEL, R: Studies onTailplane Stall for a Generic Transport AircraftWind Tunnel Model. In: Notes on NumericalFluid Mechanics and Multidisciplinary Design,Vol. 96; C. Tropea, S. Jakirlic, H.-J. Heinemann,R. Henke, H. Hönlinger; Springer, Berlin HeidelbergNew York, 2007.6. EISFELD, B. : Numerical Simulation of AerodynamicProblems with SSG/LRR-ω ReynoldsStress Turbulence Model Using the UnstructuredTAU Code. Notes on Numerical Fluid Mechanicsand Multidisciplinary Design, Vol. 96,Springer, Berlin, 2007.FundingFederal Ministry of Economics and TechnologyIngenieurwissenschaften