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

C Zwerger; Stefan Hickel; C Breitsamter; NA Adams

doi:10.1007/978-3-319-27279-5_53

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 volume › Chapter › Scientific › peer-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 language	English
Title of host publication	New Results in Numerical and Experimental Fluid Mechanics X
Subtitle of host publication	Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014
Editors	A. Dillmann, G. Heller, E. Krämer, C. Wagner, C. Breitsamter
Publisher	Springer Science+Business Media
Pages	607-616
ISBN (Electronic)	978-3-319-27279-5
ISBN (Print)	978-3-319-27278-8
DOIs	https://doi.org/10.1007/978-3-319-27279-5_53
Publication status	Published - 2016
Externally published	Yes
Event	19th STAB/DGLR Symposium - Munich, Germany Duration: 4 Nov 2014 → 5 Nov 2014 Conference number: 19

Publication series

Name	Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)
Publisher	Springer
Number	132
ISSN (Electronic)	1612-2909

Conference

Conference	19th STAB/DGLR Symposium
Country/Territory	Germany
City	Munich
Period	4/11/14 → 5/11/14

Access to Document

10.1007/978-3-319-27279-5_53

Cite this

Zwerger, C., Hickel, S., Breitsamter, C., & Adams, NA. (2016). Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge. In A. Dillmann, G. Heller, E. Krämer, C. Wagner, & C. Breitsamter (Eds.), New Results in Numerical and Experimental Fluid Mechanics X: Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014 (pp. 607-616). (Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM); No. 132). Springer Science+Business Media. https://doi.org/10.1007/978-3-319-27279-5_53

Zwerger, C ; Hickel, Stefan ; Breitsamter, C ; Adams, NA. / Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge. New Results in Numerical and Experimental Fluid Mechanics X: Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014 . editor / A. Dillmann ; G. Heller ; E. Krämer ; C. Wagner ; C. Breitsamter. Springer Science+Business Media, 2016. pp. 607-616 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM); 132).

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title = "Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge",

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 ",

author = "C Zwerger and Stefan Hickel and C Breitsamter and NA Adams",

year = "2016",

doi = "10.1007/978-3-319-27279-5_53",

language = "English",

isbn = "978-3-319-27278-8",

series = "Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)",

publisher = "Springer Science+Business Media",

number = "132",

pages = "607--616",

editor = "A. Dillmann and G. Heller and E. Kr{\"a}mer and C. Wagner and C. Breitsamter",

booktitle = "New Results in Numerical and Experimental Fluid Mechanics X",

note = "19th STAB/DGLR Symposium ; Conference date: 04-11-2014 Through 05-11-2014",

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Zwerger, C, Hickel, S, Breitsamter, C & Adams, NA 2016, Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge. in A Dillmann, G Heller, E Krämer, C Wagner & C Breitsamter (eds), New Results in Numerical and Experimental Fluid Mechanics X: Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014 . Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), no. 132, Springer Science+Business Media, pp. 607-616, 19th STAB/DGLR Symposium, Munich, Germany, 4/11/14. https://doi.org/10.1007/978-3-319-27279-5_53

Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge. / Zwerger, C; Hickel, Stefan; Breitsamter, C; Adams, NA.

New Results in Numerical and Experimental Fluid Mechanics X: Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014 . ed. / A. Dillmann; G. Heller; E. Krämer; C. Wagner; C. Breitsamter. Springer Science+Business Media, 2016. p. 607-616 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM); No. 132).

Research output: Chapter in Book/Conference proceedings/Edited volume › Chapter › Scientific › peer-review

TY - CHAP

T1 - Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge

AU - Zwerger, C

AU - Hickel, Stefan

AU - Breitsamter, C

AU - Adams, NA

N1 - Conference code: 19

PY - 2016

Y1 - 2016

N2 - 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

AB - 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

U2 - 10.1007/978-3-319-27279-5_53

DO - 10.1007/978-3-319-27279-5_53

M3 - Chapter

SN - 978-3-319-27278-8

T3 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)

SP - 607

EP - 616

BT - New Results in Numerical and Experimental Fluid Mechanics X

A2 - Dillmann, A.

A2 - Heller, G.

A2 - Krämer, E.

A2 - Wagner, C.

A2 - Breitsamter, C.

PB - Springer Science+Business Media

T2 - 19th STAB/DGLR Symposium

Y2 - 4 November 2014 through 5 November 2014

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Zwerger C, Hickel S, Breitsamter C, Adams NA. Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge. In Dillmann A, Heller G, Krämer E, Wagner C, Breitsamter C, editors, New Results in Numerical and Experimental Fluid Mechanics X: Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014 . Springer Science+Business Media. 2016. p. 607-616. (Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM); 132). https://doi.org/10.1007/978-3-319-27279-5_53

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

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