Numerical High Lift Research II
S. Melber-Wilkending,
E. Stumpf,
J. Wild and
R. Rudnik
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S. Melber-Wilkending: Transport Aircraft, DLR Braunschweig, Institute of Aerodynamics and Flow Technology
E. Stumpf: Transport Aircraft, DLR Braunschweig, Institute of Aerodynamics and Flow Technology
J. Wild: Transport Aircraft, DLR Braunschweig, Institute of Aerodynamics and Flow Technology
R. Rudnik: Transport Aircraft, DLR Braunschweig, Institute of Aerodynamics and Flow Technology
A chapter in High Performance Computing in Science and Engineering ’03, 2003, pp 315-330 from Springer
Abstract:
Summary The project NHLRes is concerned with the simulation of aircraft aerodynamics and thus belongs to the research field of computational fluid dynamics (CFD) for aerospace applications. NHLRes comprises the numerical simulation of the viscous flow around transport aircraft high lift configurations based on the solution of the Reynolds-averaged Navier-Stokes equations. The project NHLRes II, a follow-on activity of the NHLRes project [1], consists of three parts representing a analysis of complex 3D-flow features, wake vortex simulations and an optimization task for selected three-dimensional high lift flow problems.
Keywords: Vortex Pair; Wake Vortex; Rolling Moment; High Lift; Main Vortex (search for similar items in EconPapers)
Date: 2003
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-642-55876-4_24
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DOI: 10.1007/978-3-642-55876-4_24
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