Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees

Yue Wang; Kang Liu; Wenping Song; Zhonghua Han

Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees

Yue Wang, Kang Liu, Wenping Song, Zhonghua Han

School of Aeronautics

Northwestern Polytechnical University Xian

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

High Reynolds number flows around airfoils involve complex phenomena at different angles of attack (AOA). In this study, improved delayed detached eddy simulations (IDDES) are carried to investigate the flows around S809 airfoil at a wide range of AOA from 0 to 90 degrees. In addition, unsteady Reynolds-averaged Navier-Stokes simulations (URANS) are adopted for a comparison purpose. Both IDDES and URANS simulations agree well with the experimental results in the attached flow regime of low AOA. However, in the mild separation and massive separation regime, IDDES simulations show better prediction than the URANS simulations. Detailed flow structures are analyzed with comparisons between IDDES and URANS simulations.

Original language	English
Title of host publication	31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
Publisher	International Council of the Aeronautical Sciences
ISBN (Electronic)	9783932182884
State	Published - 2018
Event	31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018 - Belo Horizonte, Brazil Duration: 9 Sep 2018 → 14 Sep 2018

Publication series

Name	31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018

Conference

Conference	31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
Country/Territory	Brazil
City	Belo Horizonte
Period	9/09/18 → 14/09/18

Cite this

Wang, Y., Liu, K., Song, W., & Han, Z. (2018). Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees. In 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018 (31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018). International Council of the Aeronautical Sciences.

Wang, Yue ; Liu, Kang ; Song, Wenping et al. / Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees. 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. International Council of the Aeronautical Sciences, 2018. (31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018).

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title = "Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees",

abstract = "High Reynolds number flows around airfoils involve complex phenomena at different angles of attack (AOA). In this study, improved delayed detached eddy simulations (IDDES) are carried to investigate the flows around S809 airfoil at a wide range of AOA from 0 to 90 degrees. In addition, unsteady Reynolds-averaged Navier-Stokes simulations (URANS) are adopted for a comparison purpose. Both IDDES and URANS simulations agree well with the experimental results in the attached flow regime of low AOA. However, in the mild separation and massive separation regime, IDDES simulations show better prediction than the URANS simulations. Detailed flow structures are analyzed with comparisons between IDDES and URANS simulations.",

author = "Yue Wang and Kang Liu and Wenping Song and Zhonghua Han",

note = "Publisher Copyright: {\textcopyright} 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. All rights reserved.; 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018 ; Conference date: 09-09-2018 Through 14-09-2018",

year = "2018",

language = "英语",

series = "31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018",

publisher = "International Council of the Aeronautical Sciences",

booktitle = "31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018",

}

Wang, Y, Liu, K, Song, W & Han, Z 2018, Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees. in 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018, International Council of the Aeronautical Sciences, 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018, Belo Horizonte, Brazil, 9/09/18.

Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees. / Wang, Yue; Liu, Kang; Song, Wenping et al.
31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. International Council of the Aeronautical Sciences, 2018. (31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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T1 - Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees

AU - Wang, Yue

AU - Liu, Kang

AU - Song, Wenping

AU - Han, Zhonghua

PY - 2018

Y1 - 2018

N2 - High Reynolds number flows around airfoils involve complex phenomena at different angles of attack (AOA). In this study, improved delayed detached eddy simulations (IDDES) are carried to investigate the flows around S809 airfoil at a wide range of AOA from 0 to 90 degrees. In addition, unsteady Reynolds-averaged Navier-Stokes simulations (URANS) are adopted for a comparison purpose. Both IDDES and URANS simulations agree well with the experimental results in the attached flow regime of low AOA. However, in the mild separation and massive separation regime, IDDES simulations show better prediction than the URANS simulations. Detailed flow structures are analyzed with comparisons between IDDES and URANS simulations.

AB - High Reynolds number flows around airfoils involve complex phenomena at different angles of attack (AOA). In this study, improved delayed detached eddy simulations (IDDES) are carried to investigate the flows around S809 airfoil at a wide range of AOA from 0 to 90 degrees. In addition, unsteady Reynolds-averaged Navier-Stokes simulations (URANS) are adopted for a comparison purpose. Both IDDES and URANS simulations agree well with the experimental results in the attached flow regime of low AOA. However, in the mild separation and massive separation regime, IDDES simulations show better prediction than the URANS simulations. Detailed flow structures are analyzed with comparisons between IDDES and URANS simulations.

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M3 - 会议稿件

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T3 - 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018

BT - 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018

PB - International Council of the Aeronautical Sciences

T2 - 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018

Y2 - 9 September 2018 through 14 September 2018

ER -

Wang Y, Liu K, Song W , Han Z. Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees. In 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. International Council of the Aeronautical Sciences. 2018. (31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018).

Improved delayed detached eddy simulation of the flows around S809 airfoil for angles of attack from 0 to 90 degrees

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