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eN transition prediction for 3D wing configurations using database methods and a local, linear stability code

Krumbein, Andreas (2008) eN transition prediction for 3D wing configurations using database methods and a local, linear stability code. Aerospace Science and Technology, Vol. 1, pp. 592-598. Elsevier. DOI: 10.1016/j.ast.2008.01.005

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Official URL: http://www.sciencedirect.com/science?_ob=ArticleURL&_udi=B6VK2-4RWBT2X-1&_user=100058&_rdoc=1&_fmt=&_orig=search&_sort=d&view=c&_acct=C000007338&_version=1&_urlVersion=0&_userid=100058&md5=d8d49e2d3a46e4f247c3b7c0f86d2215

Abstract

A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition prediction methods for the prediction of Tollmien-Schlichting and cross flow instabilities were coupled in order to perform Reynolds-averaged Navier-Stokes computations of three-dimensional, finite wings with automatic laminar-turbulent transition prediction. The results from computations based on two database methods and a local, linear stability code together with the eN-method are compared for a three-dimensional wing configuration.

Item URL in elib:https://elib.dlr.de/56022/
Document Type:Article
Title:eN transition prediction for 3D wing configurations using database methods and a local, linear stability code
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krumbein, AndreasUNSPECIFIEDUNSPECIFIED
Date:November 2008
Journal or Publication Title:Aerospace Science and Technology
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 1
DOI :10.1016/j.ast.2008.01.005
Page Range:pp. 592-598
Publisher:Elsevier
Status:Published
Keywords:Transition prediction, RANS solver, eN-method, 3D wings
HGF - Research field:Aeronautics, Space and Transport
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: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > CASE
Deposited By: Krumbein, Dr.-Ing. Andreas
Deposited On:11 Nov 2008
Last Modified:12 Dec 2013 20:33

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