elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Engine Integration on Transport Aircraft - The European Research Activities on Propulsion Airframe Integration

von Geyr, H. and Brodersen, O. and Melber, S. (2001) Engine Integration on Transport Aircraft - The European Research Activities on Propulsion Airframe Integration. In: Book of Abstracts - ECCOMAS CFD 2001, 34-. ECCOMAS Computational Fluid Dynamics Conference 2001, Swansea (gb), 04.-07.09.2001. ISBN 0905091116.

Full text not available from this repository.

Abstract

Environmental demands and the need to lower DOCs force industry to reduce fuel consumption and the noise emission of the aircrafts, which lead to an installation of engines with high bypass ratio. The main objective of this paper is to present the key results of a detailed study of the numerical prediction of thrust and drag on a Airbus-type transport aircraft configuration obtained within the EU-project AIRDATA. These research activities aim to accurately predict the installation drag for engines with different bypass ratios and at different flow conditions using structured as well as unstructured / hybrid approaches of today's state-of-the-art Navier-Stokes solvers. Results of installation drag predictions on the Airbus-type ALVAST configuration with powered engines of different bypass ratios will be analyzed for different flow and thrust conditions and compared with measurements. It is demonstrated, that numerical methods are able to predict installation drag within good accuracy when the non-physical spurious drag caused by approximation and discretization errors is separated. The paper will make use of different methods for spurious drag separation, such as force extrapolation to zero mesh size and spurious drag evaluation. The increasing complexity of the configurations turns structured mesh generation into a very complex, time and labour consuming process. Within this paper the capability of hybrid methods in combination with appropriate mesh adaptation techniques for accurate prediction of installation drag will be demonstrated. These investigations are performed at DLR on the DLR-F6 civil transport aircraft configuration. The results clearly show, that hybrid Navier-Stokes methods are capable to predict the installation drag with a good accuracy.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2002,
Title:Engine Integration on Transport Aircraft - The European Research Activities on Propulsion Airframe Integration
Authors:
AuthorsInstitution or Email of Authors
von Geyr, H.UNSPECIFIED
Brodersen, O.UNSPECIFIED
Melber, S.UNSPECIFIED
Date:2001
Journal or Publication Title:Book of Abstracts - ECCOMAS CFD 2001
Page Range:34-
ISBN:0905091116
Status:Published
Keywords:CFD, powered engine, drag prediction, mesh generation
Event Title:ECCOMAS Computational Fluid Dynamics Conference 2001, Swansea (gb), 04.-07.09.2001
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
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:31 Jan 2006
Last Modified:14 Jan 2010 18:53

Repository Staff Only: item control page

Browse
Search
Help & Contact
Informationen
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.