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Extension of a Reynolds-Stress-Based Transition Transport Model for Crossflow Transition

Nie, Shengyang and Krimmelbein, Normann and Krumbein, Andreas and Grabe, Cornelia (2018) Extension of a Reynolds-Stress-Based Transition Transport Model for Crossflow Transition. Journal of Aircraft, Vol.55 (No. 4), pp. 1641-1654. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C034586 ISSN 0021-8669

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Official URL: https://doi.org/10.2514/1.C034586


Item URL in elib:https://elib.dlr.de/121680/
Document Type:Article
Additional Information:Dieser Journalartikel wurde begutachtet: Peer-Review mit 3 Gutachtern. Das angehängte PDF ist die Postprint-Version des Artikels vor der endgültigen Annahme durch das Journal of Aircraft.
Title:Extension of a Reynolds-Stress-Based Transition Transport Model for Crossflow Transition
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Nie, Shengyangniesynpu (at) hotmail.comUNSPECIFIED
Krimmelbein, Normannnormann.krimmelbein (at) dlr.deUNSPECIFIED
Krumbein, AndreasAndreas.Krumbein (at) dlr.dehttps://orcid.org/0000-0002-2772-7328
Grabe, Corneliacornelia.grabe (at) dlr.deUNSPECIFIED
Date:July 2018
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:Vol.55
DOI :10.2514/1.C034586
Page Range:pp. 1641-1654
Editors:
EditorsEmail
UNSPECIFIEDAmerican Institute of Aeronautics and Astronautics
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0021-8669
Status:Published
Keywords:Transition transport modeling, DLR TAU code, RANS, transition prediction, Langtry, Menter, Reynolds stress model, RSM, SSG/LRR, γ−Reθt model, coupling with RSM, crossflow extension, C1-based Approach, helicity-based Approach, NLF(2)-0415, DLR 6:1 spheroid, DLR-F4 wing-body, validation
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: Braunschweig , Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > CASE, BS
Institute for Aerodynamics and Flow Technology > CASE, GO
Deposited By: Krumbein, Dr.-Ing. Andreas
Deposited On:13 Sep 2018 09:15
Last Modified:17 Sep 2018 15:37

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