Landa, Tim und Klug, Lorenz und Radespiel, Rolf und Probst, Silvia und Knopp, Tobias (2018) Experimental and Numerical Analysis of a Streamwise Vortex Downstream of a Delta Wing. In: 48th AIAA Fluid Dynamics Conference. 48th Fluid Dynamics Conference 2018, AIAA AVIATION Forum, (AIAA 2018-4157), 2018-06-25 - 2018-06-29, Atlanta, USA. doi: 10.2514/6.2018-4157. ISBN 978-162410553-1. ISSN 2018-4157.
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Offizielle URL: https://arc.aiaa.org/doi/10.2514/6.2018-4157
Kurzfassung
The present paper analyzes the vortical flow downstream of a delta wing. The Delta wing is designed to generate a vortex which resembles the vortex of a nacelle strake. The experimental results of stereo-PIV measurements performed at different positions downstream of the delta wing display the streamwise development of the vortex. The distributions of the mean axial and tangential velocity components and Reynolds-stresses characterize the vortex development. In addition, results of numerical simulations with the DLR TAU-code applying the Menter-SST eddy viscosity model and the SSG/LRR-Omega Reynolds-Stress model show the ability of the turbulence models to capture the vortex development. The experimental results indicate a preservation of the vortex strength and structure downstream of the delta wing. The Menter-SST model does not predict this preservation, rather it computes a rapid decay of the vortex strength and an increase of the vortex size. In contrast, the results of the SSG/LRR-Omega model are in good Agreement with the experiments concerning the mean flow development. However, turbulence in the vortex core is underpredicted by both turbulence models.
elib-URL des Eintrags: | https://elib.dlr.de/121858/ | ||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
Titel: | Experimental and Numerical Analysis of a Streamwise Vortex Downstream of a Delta Wing | ||||||||||||||||||||||||
Autoren: |
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Datum: | 2018 | ||||||||||||||||||||||||
Erschienen in: | 48th AIAA Fluid Dynamics Conference | ||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
DOI: | 10.2514/6.2018-4157 | ||||||||||||||||||||||||
ISSN: | 2018-4157 | ||||||||||||||||||||||||
ISBN: | 978-162410553-1 | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | Delta Wing, Strake Vortex, CFD, Experiment,vwind tunnel Experiment; PIV; RSM | ||||||||||||||||||||||||
Veranstaltungstitel: | 48th Fluid Dynamics Conference 2018, AIAA AVIATION Forum, (AIAA 2018-4157) | ||||||||||||||||||||||||
Veranstaltungsort: | Atlanta, USA | ||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
Veranstaltungsbeginn: | 25 Juni 2018 | ||||||||||||||||||||||||
Veranstaltungsende: | 29 Juni 2018 | ||||||||||||||||||||||||
Veranstalter : | AIAA | ||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | Flugzeuge | ||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation und Validierung (alt) | ||||||||||||||||||||||||
Standort: | Göttingen | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > CASE, GO | ||||||||||||||||||||||||
Hinterlegt von: | Probst, Dr. Silvia | ||||||||||||||||||||||||
Hinterlegt am: | 07 Nov 2018 15:16 | ||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:25 |
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