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

MEGAFLOW - Numerical Flow Simulation for Aircraft Design Results of the second phase of the German CFD initiative MEGAFLOW, presented during its closing syposium at DLR, Braunschweig, Germany, December 10 and 11, 2002

Kroll, N. and Faßbender, J.K. (2005) MEGAFLOW - Numerical Flow Simulation for Aircraft Design Results of the second phase of the German CFD initiative MEGAFLOW, presented during its closing syposium at DLR, Braunschweig, Germany, December 10 and 11, 2002. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89. 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

This volume contains results of the German CFD initiative MEGAFLOW which combines many of the CFD development activities from DLR, universities and aircraft industry. It high-lights recent improvements and enhancement of the MEGAFLOW software system. This software system includes the block-structured Navier-Stokes code FLOWer and the unstructured Navier-Stokes code TAU. Besides improvments to numerical algorithms and physical modelling capabilities of these codes the validation of their capability to predict viscous flows around complex industrial applications for transport aircraft design is presented. This documents the high level of maturity both codes have reached. The goal of MEGAFLOW to develop and validate dependable and efficient numerical tools for the aerodynamic simulation of complete aircraft is proven based on the intensive use of FLOWer and TAU by the German aerospace industry in the design process of a new aircraft.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005,
Title:MEGAFLOW - Numerical Flow Simulation for Aircraft Design Results of the second phase of the German CFD initiative MEGAFLOW, presented during its closing syposium at DLR, Braunschweig, Germany, December 10 and 11, 2002
Authors:
AuthorsInstitution or Email of Authors
Kroll, N.UNSPECIFIED
Faßbender, J.K.UNSPECIFIED
Date:2005
Journal or Publication Title:MEGAFLOW - Numerical Flow Simulation for Aircraft Design
Volume:89
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:Computational Fluid Dynamics (CFD), Structured and hybrid Navier-Stokes solvers, aerodynamic shape optimization
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 19:50

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.