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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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Abstract
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/ | |||||||||
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| 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 | |||||||||
| Authors: |
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| Date: | 2017 | |||||||||
| Refereed publication: | No | |||||||||
| Open Access: | No | |||||||||
| Gold Open Access: | No | |||||||||
| In SCOPUS: | No | |||||||||
| In ISI Web of Science: | No | |||||||||
| Status: | Published | |||||||||
| 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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