Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge

C Zwerger, Stefan Hickel, C Breitsamter, NA Adams

Research output: Chapter in Book/Conference proceedings/Edited volumeChapterScientificpeer-review

Abstract

We performed wall modeled large eddy simulation of the flow field around a delta wing with sweep angle of 65 ∘ and round leading edge at angles of attack of 13∘ , 18 ∘ , and 23 ∘ . Qualitatively, the numerical simulations correctly predict the flow phenomena for all angles of attack considered. Quantitatively, the results show reasonable agreement with experimental measurements of steady and unsteady surface pressures, velocity distributions, and vortex breakdown position and frequency
Original languageEnglish
Title of host publicationNew Results in Numerical and Experimental Fluid Mechanics X
Subtitle of host publicationContributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014
EditorsA. Dillmann, G. Heller, E. Krämer, C. Wagner, C. Breitsamter
PublisherSpringer
Pages607-616
ISBN (Electronic)978-3-319-27279-5
ISBN (Print)978-3-319-27278-8
DOIs
Publication statusPublished - 2016
Externally publishedYes
Event19th STAB/DGLR Symposium - Munich, Germany
Duration: 4 Nov 20145 Nov 2014
Conference number: 19

Publication series

NameNotes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)
PublisherSpringer
Number132
ISSN (Electronic)1612-2909

Conference

Conference19th STAB/DGLR Symposium
CountryGermany
CityMunich
Period4/11/145/11/14

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