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Airbus, ONERA, and DLR Results from the Second AIAA Drag Prediction Workshop

Brodersen, Olaf and Rakowitz, Mark and Amant, Stephane and Larrieu, Pascal and Destarac, Daniel and Sutcliffe, Mark (2005) Airbus, ONERA, and DLR Results from the Second AIAA Drag Prediction Workshop. Journal of Aircraft, 42 (4), pp. 932-940. ISSN 0021-8669.

Full text not available from this repository.

Official URL: http://www.aiaa.org

Abstract

The results from DLR, Airbus, and ONERA from the Second AIAA Computational Fluid Dynamics Drag Prediction Workshop are presented. The lift, drag, and pitching moments are calculated for the DLR-F6 configuration at transonic flow conditions by solving the Reynolds-averaged Navier-Stokes equations on structured as well as on unstructured, hybrid grids.

Item URL in elib:https://elib.dlr.de/19695/
Document Type:Article
Title:Airbus, ONERA, and DLR Results from the Second AIAA Drag Prediction Workshop
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Brodersen, OlafUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Rakowitz, MarkUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Amant, StephaneAirbus FranceUNSPECIFIEDUNSPECIFIED
Larrieu, PascalAirbus FranceUNSPECIFIEDUNSPECIFIED
Destarac, DanielONERAUNSPECIFIEDUNSPECIFIED
Sutcliffe, MarkAirbus DeutschlandUNSPECIFIEDUNSPECIFIED
Date:2 July 2005
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:42
Page Range:pp. 932-940
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
AIAA, UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
ISSN:0021-8669
Status:Published
Keywords:Numerical Aerodynamics, Navier-Stokes, CFD, DLR-F6, Validation, TAU
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: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Brodersen, Dr.-Ing. Olaf
Deposited On:25 Jan 2006
Last Modified:27 Apr 2009 04:43

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