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

Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code

Schütte, Andreas and Lüdeke, Heinrich (2013) Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code. Aerospace Science and Technology, 24 (1), pp. 56-65. Elsevier. DOI: [10.1016/j.ast.2012.03.002] ISSN 1270-9638

Full text not available from this repository.

Official URL: http://www.sciencedirect.com/science/article/pii/S1270963812000648/pdfft?md5=8f7eaccbd91c9e186957fc147d2d1743&pid=1-s2.0-S1270963812000648-main.pdf

Abstract

The numerical simulation of the flow around a 65◦ delta wing configuration with rounded leading edges is presented. For the numerical simulation the DLR TAU-Code is used which is based on an unstructured hybrid mesh approach. Within this paper several numerical results are shown, solving the steady RANS equations by different turbulence models. The simulations are carried out within the RTO/AVT-113 task group focusing on experimental and numerical research on delta wing configurations with rounded leading edges. Within this paper the focus is related to the flow topology depending on the angle of attack as well as on Reynolds number effects. Finally the results are compared and verified by experimental data.

Item URL in elib:https://elib.dlr.de/86555/
Document Type:Article
Title:Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schütte, AndreasAndreas.Schuette (at) dlr.deUNSPECIFIED
Lüdeke, Heinrichheinrich.luedeke (at) dlr.deUNSPECIFIED
Date:2013
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:24
DOI :[10.1016/j.ast.2012.03.002]
Page Range:pp. 56-65
Editors:
EditorsEmail
Hummel, Dietrichdietrich.hummel@tu-braunschweig.de
Cummings, Russel M.russ.cummings@usafa.edu
Publisher:Elsevier
Series Name:Aerospace Science and Technology
ISSN:1270-9638
Status:Published
Keywords:Vortical flow Delta wing Blunt leading edge Experiments Numerics CFD DES RTO VFE-2 AVT TAU-Code DLR
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 - Military Technologies (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Schütte, Andreas
Deposited On:10 Dec 2013 15:15
Last Modified:10 Jan 2019 15:45

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.