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One-Equation Transition Model for Airfoil and Wing Aerodynamics

Fehrs, Michael (2018) One-Equation Transition Model for Airfoil and Wing Aerodynamics. In: New Results in Numerical and Experimental Fluid Mechanics XI, 136, pp. 199-208. Springer. 20. DGLR-Fach-Symposium der STAB, 08.-09. Nov. 2016, Braunschweig, Deutschland. DOI: 10.1007/978-3-319-64519-3 ISBN 978-3-319-64518-6 ISSN 1612-2909

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Item URL in elib:https://elib.dlr.de/107779/
Document Type:Conference or Workshop Item (Speech)
Title:One-Equation Transition Model for Airfoil and Wing Aerodynamics
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fehrs, Michaelmichael.fehrs (at) dlr.deUNSPECIFIED
Date:2018
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics XI
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:136
DOI :10.1007/978-3-319-64519-3
Page Range:pp. 199-208
Editors:
EditorsEmail
Dillmann, AndreasDLR
Heller, GerdAirbus Deutschland
Krämer, EwaldUniversität Stuttgart
Wagner, ClausDLR
Bansmer, StephanTU Braunschweig
Radespiel, RolfTU Braunschweig
Semaan, RichardTU Braunschweig
Publisher:Springer
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-319-64518-6
Status:Published
Keywords:boundary layer transition, CFD, transition model
Event Title:20. DGLR-Fach-Symposium der STAB
Event Location:Braunschweig, Deutschland
Event Type:national Conference
Event Dates:08.-09. Nov. 2016
Organizer:DGLR
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Aeroelastic Simulation
Deposited By: Fehrs, Michael
Deposited On:09 Dec 2016 09:28
Last Modified:22 May 2018 10:25

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