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An Inverse Design Method for Designing Isolated and Wing-Mounted Engine Nacelles

Wilhelm, R. (2002) An Inverse Design Method for Designing Isolated and Wing-Mounted Engine Nacelles. 40th Aerospace Sciences Meeting and Exhibit, Reno (usa), 14.-17.01.2002.

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Because of the time-consuming process of generating complex block-structured grids and because of the achieved results in the field of computational fluid dynamics methods using arbitrary grids, an inverse design system has been developed that is capable of handling flowfield calculations on arbitrary grids. The flow solver used is the DLR-TAU code, a finite volume flow solver for the solution of the Reynolds averaged Navier-Stokes equations on hybrid grids. The inverse design method is based on an iterative residual-correction-type approach to generate a geometry that satisfies a user-precribed target pressure distribution. The design method has been adapted for the design of isolated and wing-mounted engine nacelles. Results are presented for the inverse design of isolated three-dimensional nacelles and wing-mounted engine nacelles considering the pylon. The baseline aircraft is the DLR ALVAST configuration.

Item URL in elib:https://elib.dlr.de/12532/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2003,
Title:An Inverse Design Method for Designing Isolated and Wing-Mounted Engine Nacelles
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:inverse design system, DLR TAU code, engine nacelles, DLR ALVAST configuration
Event Title:40th Aerospace Sciences Meeting and Exhibit, Reno (usa), 14.-17.01.2002
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts & Integration (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Grant, Claudia
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:07

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