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Application of the EADS-M Mesher to a Transonic and a Supersonic Aircraft in High-Lift Configuration

Schweikhard, R. (2005) Application of the EADS-M Mesher to a Transonic and a Supersonic Aircraft in High-Lift Configuration. DLR-Interner Bericht. 124-2005/912, 16 S.

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Abstract

The EADS-M Mesher, which is still under development, is capable of generating hybrid unstructured meshes. Features and handling are comparable to the Centaur mesh generator. The EADS-M Mesher is applied to two different wing-body high-lift configurations: a transonic and a supersonic one. It turns out that the EADS-M Mesher produces high-quality meshes and enables a good control over mesh features.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Application of the EADS-M Mesher to a Transonic and a Supersonic Aircraft in High-Lift Configuration
Authors:
AuthorsInstitution or Email of Authors
Schweikhard, R.UNSPECIFIED
Date:2005
Number of Pages:16
Status:Published
Keywords:Mesh Generation, Grid Generation, Netzgenerierung
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Claudia Grant
Deposited On:09 Oct 2005
Last Modified:14 Jan 2010 20:00

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