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Requirements and Challenges for Transition Modeling in CFD

Krumbein, Andreas and Krimmelbein, Normann (2017) Requirements and Challenges for Transition Modeling in CFD. NASA Transition Modeling Workshop, Lockheed Martin Innovation Center, 13. Sep. 2017, Suffolk (Virginia), USA.

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Übersichtsvortrag zum Stand der CFD-Transitionsmodellierung am Institut AS in der Abteilung C2A2S2E und den derzeitigen und künftigen Anforderungen, Problembereichen und Zielsetzungen

Item URL in elib:https://elib.dlr.de/114347/
Document Type:Conference or Workshop Item (Speech)
Additional Information:https://turbmodels.larc.nasa.gov/Transition_workshop2017/transition_workshop2017_agenda.pdf
Title:Requirements and Challenges for Transition Modeling in CFD
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Krumbein, AndreasUNSPECIFIEDhttps://orcid.org/0000-0002-2772-7328
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:physical modeling, transition modeling, simulation, transition prediction, eN-method, complete flight envelope, virtual product, virtual aircraft, CFD, RANS solver, DLR TAU code, streamlines, unstructured, validation, complex configuration, A320, linear stability theory, transition criteria, 2-N factor method, integration paths, gamma-Re,theta-CF model, TU Braunschweig sickle wing, 6:1 prolate spheroid, DLR-F4 wing-body, coupling to Reynolds stress model, complex 3D test cases, helicity-based transition criterion, crossflow transition, hybrid-laminar flow control
Event Title:NASA Transition Modeling Workshop, Lockheed Martin Innovation Center
Event Location:Suffolk (Virginia), USA
Event Type:Workshop
Event Dates:13. Sep. 2017
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 (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > CASE, GO
Institute for Aerodynamics and Flow Technology > CASE, BS
Deposited By: Bachmann, Barbara
Deposited On:22 Sep 2017 12:32
Last Modified:22 Sep 2017 12:32

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