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MEGAFLOW - A numerical Simulation Tool for Aircraft Design

Kroll, N. and Heinrich, R. (2004) MEGAFLOW - A numerical Simulation Tool for Aircraft Design. JAXA ANSS2004 (Aerospace Numerical Simulation Symposium), Tokyo (ja), 24.-25.06.2004.

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Some years ago the national CFD project MEGAFLOW was initiated in Germany, which combines many of the CFD development activities from DLR, universities and aircraft industry. Its goal is the development and validation of a dependable and efficient numerical tool for the aerodynamic simulation of complete aircraft. The MEGAFLOW software system includes the blockstructured Navier-Stokes code FLOWer and the unstructured Navier-Stokes code TAU. Both codes have reached a high level of maturity and they are being intensively used by the German aerospace industry in the design process of a new aircraft. This paper highlights recent improvements and enhancements of the software. Its capability to predict viscous flows around complex industrial applications for transport aircraft design is demonstrated.

Item URL in elib:https://elib.dlr.de/12944/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005,
Title:MEGAFLOW - A numerical Simulation Tool for Aircraft Design
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Euler, RANS, MEGAFLOW
Event Title:JAXA ANSS2004 (Aerospace Numerical Simulation Symposium), Tokyo (ja), 24.-25.06.2004
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 19:43

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