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.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Similar content being viewed by others
References
Rudnik, R.; Ronzheimer, A.; Raddatz, J.: “Numerical Flow Simulation for a Wing/Fuselage Transport Configuration with Deployed High Lift system” in Notes on Numerical Fluid Mechanics, Vol. 72, pp. 363–370, Vieweg-Verlag, Braunschweig/Wiesbaden, 1999.
Rudnik, R.; Melber, S.; Ronzheimer, A.; Brodersen, O.: “Three-Dimensional Navier-Stokes Simulations for Transport Aircraft High Lift Configurations.” Journal of Aircraft, Vol. 38, pp. 895–903, 2001.
Melber, S.; Rudnik, R.; Ronzheimer, A.: “Structured and Unstructured Numerical Simulation in High Lift Aerodynamics.” Workshop on EU-Research on Aerodynamic Engine/Aircraft Integration for Transport Aircraft,27 September 2000, DLR Braunschweig, 2000, pp. 13-1–13-10.
Melber, S.: “3D RANS Simulations for High Lift Analysis of Transport Aircraft Configurations.” Notes on numerical fluid mechanics, Volume 77, Springer Verlag, Berlin, Heidelberg, New York, 2002, pp. 27–34.
Rogers, S.E.; Roth, K.; Cao, V.Hoa; Slotnick, J.R; Whilock, M.; Nash, S.M.; Baker, M.D.: “Computation of viscous Flow for a Boeing 777 Aircraft in Landing Conf.” AIAA paper 2000 - 4221, 2000.
Mavriplis, D.J.: “Parallel Performance Investigations of an Unstructured Mesh Navier-Stokes Solver” ICASE Report No. 2000 - 13, March 2000.
Kiock, R.: “The ALVAST Model of DLR” DLR IB 129-96/22, 1996
Kallinderis, Y.: “Hybrid Grids and Their Applications.” Handbook of Grid Generation, CRC Press, Boca Raton/London/New York/Washington, D.C., pp. 25-1–25 - 18, 1999
Puffert-Meissner, W .: “ALVAST Half-Model Investigations in the Low-Speed wind-tunnel Braunschweig” DLR IB 129-95/11, 1995
Puffert-Meissner, W.: “ALVAST Half-Model wind-tunnel Investigations and Comparison with Full-Span Model Results.” DLR IB 129-96/20, 1996
Kroll, N.; Rossow, C.-C.; Becker, K.; Thiele, F.: “MEGAFLOW–A Numerical Flow Simulation System.” 21st ICAS congress, 1998, Melbourne, 13.9.– 18.9.1998, ÏCAS-98-2. 7. 4, 1998.
Earnshaw, P.B.; Green, A.R.; Hardy, B.C.; Jelly, A.H.: “A Study of the use of Half-Models in High-Lift Wind-Tunnel Testing.” AGARD CP 515, Paper 20, 1993.
Milholen II, W.E.: “A Design Methodology for Semi-Span Model Mounting Geometries.” AIAA-paper 98 - 0758, 1998.
Haines, A.B.: “Scale Effects on Aircraft and Weapon Aerodynamics.” AGAR- Dograph 323, 1994, pp. 63.-65.
Radespiel, R.; Türkei, E.; Kroll, N.: “Assessment of Preconditioning Methods.” DLR IB 95/29, 1995.
Wild, J.: “Numerische Optimierung von zweidimensionalen Hochauftriebssystemen durch Lösung der Navier-Stokes-Gleichungen” PhD-Thesis, TU Braunschweig, published as DLR-FB 2001 - 11, 2001.
Johnson, P.L.; Jones, K.M.; Madson M.D.: “Experimental Investigation of a Simplified 3D High Lift Configuration in Support of CFD Validation” AIAA Paper 2000 - 4217, 2000.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2003 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Melber, S., Wild, J., Rudnik, R. (2003). Numerical High Lift Research — NHLRes Annual Review 2001. In: Krause, E., Jäger, W. (eds) High Performance Computing in Science and Engineering ’02. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-59354-3_33
Download citation
DOI: https://doi.org/10.1007/978-3-642-59354-3_33
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-63947-0
Online ISBN: 978-3-642-59354-3
eBook Packages: Springer Book Archive