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Detached eddy simulation compared with wind tunnel results of a delta wing with sharp leading edge and vortex breakdown

  • Aerodynamics and Methods Cassidian

Publikation: Beitrag in Buch/Bericht/Konferenzband › Konferenzbeitrag › Begutachtung

6 Zitate (Scopus)

Abstract

A delta wing configuration with a sweep angle of 65° has been investigated numerically by detached eddy simulation and compared to experimental results. In the simulations different refinement settings of the grid as well as time different time step sizes have been applied in order to reproduce the formation of the primary vortex correctly. For the comparison experimental data is available from steady and unsteady surface pressure measurements, hot wire anemometry and several other measurement techniques.

OriginalspracheEnglisch
Titel30th AIAA Applied Aerodynamics Conference 2012
Herausgeber (Verlag)American Institute of Aeronautics and Astronautics Inc.
Seiten2392-2402
Seitenumfang11
ISBN (Print)9781624101854
DOIs
PublikationsstatusVeröffentlicht - 2012
Veranstaltung30th AIAA Applied Aerodynamics Conference 2012 - New Orleans, LA, USA/Vereinigte Staaten
Dauer: 25 Juni 2012 → 28 Juni 2012

Publikationsreihe

Name30th AIAA Applied Aerodynamics Conference 2012

Konferenz

Konferenz30th AIAA Applied Aerodynamics Conference 2012
Land/GebietUSA/Vereinigte Staaten
OrtNew Orleans, LA
Zeitraum25/06/12 → 28/06/12

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