Aspects of 3D RANS simulations for transport aircraft high lift configurations
Author:
Affiliation:
1. German Aerospace Center, Inst. of Design Aerodynamics, Braunschweig, Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4326
Reference19 articles.
1. Larsson, T. Separated And High-Lift Flows Over Single And Multi-Element Airfoils. ICAS-94-5.7.3,pp.2505-2518,1994
2. Lindblad, I.A.A., deCock,K.M.J. CFDPredicition of Maximum Lift of a 2D High Lift Configuration.AIAA-paper 99-3180,1999
3. Cao,H. V.,Su,T.Y.,Rogers,S.E.Navier-Stokes Analyses Of A 747 High Lift Configuration. AIAA-paper 98-2623,1998
4. Rudnik,R.,Ronzheimer,A.,Raddatz,J.Numerical Flow Simulationfor a Wing/Fuselage Transport Configuration with Deployed High-Lift System, inNotes on Numerical Fluid Mechanics, Vol.72, pp.363-370, Vieweg-Verlag, Braunschweig/Wiesbaden, 1999,Proceedings of the llth AGSTAB/DGLR SymposiumBerlin, 1998
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