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Computation of Engine-Airframe Installation Drag

Brodersen, O. (2005) Computation of Engine-Airframe Installation Drag. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 151-161. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6.

Full text not available from this repository.

Abstract

It is demonstrated that the unstructured, hybrid method of the MEGAFLOW project is capable to compute the engine-airframe installation drag for several engine types although drag differences for varying engine positions can be very small. Results are presented for the DLR-F6 and ALVAST configurations with through-flow nacelles and powered engines. Verification by grid refinement as well as validation with wind tunnel data completes this investigation.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Computation of Engine-Airframe Installation Drag
Authors:
AuthorsInstitution or Email of Authors
Brodersen, O.UNSPECIFIED
Date:2005
Journal or Publication Title:MEGAFLOW - Numerical Flow Simulation for Aircraft Design
Volume:89
Page Range:pp. 151-161
Editors:
EditorsEmail
Kroll, N.UNSPECIFIED
Faßbender, J.K.UNSPECIFIED
Publisher:Springer Verlag
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)
ISBN:3-540-24383-6
Status:Published
Keywords:MEGAFLOW, CFD
Event Title:Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002
Organizer:DLR
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 19:51

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