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Autor(en):
T. Di Fabbio, E. Tangermann, M. Klein, S. Ketterl, A. Winkler
Zusammenfassung:
The vortex dominated flow around the triple-delta wing aircraft model ADS-NA2-W1 is investigated comparing RANS with scale-resolving DDES results. The Spalart-Allmaras One-Equation Model with corrections for negative turbulent viscosity and Rotation/Curvature (SA-negRC) is employed to close the RANS equations, whereas in the scale-resolving computations the SA-based DDES model is applied. The TAU-Code solver developed by the German Aerospace Center (DLR) is employed in order to perform the numerical simulations. The solutions achieved in the current work are compared with the experimental data provided by Airbus Defence and Space. The aim is a better understanding of the vortex-dominated flows particularly in the transonic speed range in order to determine the range of the suitability of current CFD methods.
Veranstaltung:
Deutscher Luft- und Raumfahrtkongress 2020
Verlag, Ort:
Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2020
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 11 Seiten
URN:
urn:nbn:de:101:1-2020091812575627469052
DOI:
10.25967/530052
Stichworte zum Inhalt:
RANS, Hybrid RANS LES, SA turbulence model, ADS-NA2-W1 delta wing, vortex formation, vortex breakdown
Verfügbarkeit:
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Zitierform:
Di Fabbio, T.; Tangermann, E.; et al. (2020): Comparative Scale-Resolving and RANS Simulations of a Delta Wing Configuration. Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.. (Text). https://doi.org/10.25967/530052. urn:nbn:de:101:1-2020091812575627469052.
Veröffentlicht am:
18.09.2020