Numerical High Lift Research — NHLRes Annual Review 2001

S. Melber, J. Wild and R. Rudnik
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S. Melber: DLR Braunschweig, Institute of Aerodynamics and Flow Technology, Section Transport Aircraft
J. Wild: DLR Braunschweig, Institute of Aerodynamics and Flow Technology, Section Transport Aircraft
R. Rudnik: DLR Braunschweig, Institute of Aerodynamics and Flow Technology, Section Transport Aircraft

A chapter in High Performance Computing in Science and Engineering ’02, 2003, pp 406-421 from Springer

Abstract: Abstract 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 compressible flow around transport aircraft high lift configurations. The investigations are based on the solution of the Reynolds-averaged Navier-Stokes equations using a finite volume parallel solution algorithm with an unstructured data concept. The project consists of two parts representing a typical analysis as well as an optimization task for selected three-dimensional high lift flow problems.

Keywords: Computational Fluid Dynamic; High Lift; Transport Aircraft; High Lift System; Viscous Compressible Flow (search for similar items in EconPapers)
Date: 2003
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-642-59354-3_33

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DOI: 10.1007/978-3-642-59354-3_33

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