A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed

Ke Deng; Jinping Li; Gang Wang; Guangming Zhang; Zhiqing Bai; Lu Yang

doi:10.1117/12.2681299

A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed

Ke Deng, Jinping Li, Gang Wang, Guangming Zhang, Zhiqing Bai, Lu Yang

COLLEGE OF ELECTRICAL ENGINEERING AND CONTROL SCIENCE

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

Abstract

At present, the simulation scheme of grid strategy parameters at hypersonic speed is a hot topic and can be applied to the NACA0012 airfoil, but the selection criteria for Reynolds number and aspect ratio near impact are relatively few, and further research is needed. In this paper, using the NACA4 digital generator airfoil modeling method, a two-dimensional outflow field based on the sharp trailing edge NACA0012 is established. Simulation calculations obtain the numerical results. Through comparison with the reference data, a grid strategy parameters simulation scheme is presented. Unlike blunt bodies, the longitudinal and transverse ratios between cell Reynolds number and cells near impact should be no greater than 16 and 240, respectively.

Original language	English
Title of host publication	International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023
Editors	Xin Feng, Aniruddha Bhattacharjya
Publisher	SPIE
ISBN (Electronic)	9781510665040
DOIs	https://doi.org/10.1117/12.2681299
State	Published - 2023
Event	2023 International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023 - Guangzhou, China Duration: 17 Feb 2023 → 19 Feb 2023

Publication series

Name	Proceedings of SPIE - The International Society for Optical Engineering
Volume	12645
ISSN (Print)	0277-786X
ISSN (Electronic)	1996-756X

Conference

Conference	2023 International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023
Country/Territory	China
City	Guangzhou
Period	17/02/23 → 19/02/23

Keywords

NACA0012 airfoil
grid strategy parameters
hypersonic speed

Access to Document

10.1117/12.2681299

Cite this

Deng, K., Li, J., Wang, G., Zhang, G., Bai, Z., & Yang, L. (2023). A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed. In X. Feng, & A. Bhattacharjya (Eds.), International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023 Article 126454N (Proceedings of SPIE - The International Society for Optical Engineering; Vol. 12645). SPIE. https://doi.org/10.1117/12.2681299

Deng, Ke ; Li, Jinping ; Wang, Gang et al. / A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed. International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023. editor / Xin Feng ; Aniruddha Bhattacharjya. SPIE, 2023. (Proceedings of SPIE - The International Society for Optical Engineering).

@inproceedings{63fa93e68d0543ad89ae5b0c44b2355e,

title = "A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed",

abstract = "At present, the simulation scheme of grid strategy parameters at hypersonic speed is a hot topic and can be applied to the NACA0012 airfoil, but the selection criteria for Reynolds number and aspect ratio near impact are relatively few, and further research is needed. In this paper, using the NACA4 digital generator airfoil modeling method, a two-dimensional outflow field based on the sharp trailing edge NACA0012 is established. Simulation calculations obtain the numerical results. Through comparison with the reference data, a grid strategy parameters simulation scheme is presented. Unlike blunt bodies, the longitudinal and transverse ratios between cell Reynolds number and cells near impact should be no greater than 16 and 240, respectively.",

keywords = "NACA0012 airfoil, grid strategy parameters, hypersonic speed",

author = "Ke Deng and Jinping Li and Gang Wang and Guangming Zhang and Zhiqing Bai and Lu Yang",

note = "Publisher Copyright: {\textcopyright} 2023 SPIE.; 2023 International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023 ; Conference date: 17-02-2023 Through 19-02-2023",

year = "2023",

doi = "10.1117/12.2681299",

language = "英语",

series = "Proceedings of SPIE - The International Society for Optical Engineering",

publisher = "SPIE",

editor = "Xin Feng and Aniruddha Bhattacharjya",

booktitle = "International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023",

address = "美国",

}

Deng, K, Li, J, Wang, G, Zhang, G, Bai, Z & Yang, L 2023, A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed. in X Feng & A Bhattacharjya (eds), International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023., 126454N, Proceedings of SPIE - The International Society for Optical Engineering, vol. 12645, SPIE, 2023 International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023, Guangzhou, China, 17/02/23. https://doi.org/10.1117/12.2681299

A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed. / Deng, Ke; Li, Jinping; Wang, Gang et al.
International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023. ed. / Xin Feng; Aniruddha Bhattacharjya. SPIE, 2023. 126454N (Proceedings of SPIE - The International Society for Optical Engineering; Vol. 12645).

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

TY - GEN

T1 - A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed

AU - Deng, Ke

AU - Li, Jinping

AU - Wang, Gang

AU - Zhang, Guangming

AU - Bai, Zhiqing

AU - Yang, Lu

PY - 2023

Y1 - 2023

N2 - At present, the simulation scheme of grid strategy parameters at hypersonic speed is a hot topic and can be applied to the NACA0012 airfoil, but the selection criteria for Reynolds number and aspect ratio near impact are relatively few, and further research is needed. In this paper, using the NACA4 digital generator airfoil modeling method, a two-dimensional outflow field based on the sharp trailing edge NACA0012 is established. Simulation calculations obtain the numerical results. Through comparison with the reference data, a grid strategy parameters simulation scheme is presented. Unlike blunt bodies, the longitudinal and transverse ratios between cell Reynolds number and cells near impact should be no greater than 16 and 240, respectively.

AB - At present, the simulation scheme of grid strategy parameters at hypersonic speed is a hot topic and can be applied to the NACA0012 airfoil, but the selection criteria for Reynolds number and aspect ratio near impact are relatively few, and further research is needed. In this paper, using the NACA4 digital generator airfoil modeling method, a two-dimensional outflow field based on the sharp trailing edge NACA0012 is established. Simulation calculations obtain the numerical results. Through comparison with the reference data, a grid strategy parameters simulation scheme is presented. Unlike blunt bodies, the longitudinal and transverse ratios between cell Reynolds number and cells near impact should be no greater than 16 and 240, respectively.

KW - NACA0012 airfoil

KW - grid strategy parameters

KW - hypersonic speed

UR - http://www.scopus.com/inward/record.url?scp=85163298418&partnerID=8YFLogxK

U2 - 10.1117/12.2681299

DO - 10.1117/12.2681299

M3 - 会议稿件

AN - SCOPUS:85163298418

T3 - Proceedings of SPIE - The International Society for Optical Engineering

BT - International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023

A2 - Feng, Xin

A2 - Bhattacharjya, Aniruddha

PB - SPIE

T2 - 2023 International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023

Y2 - 17 February 2023 through 19 February 2023

ER -

Deng K, Li J, Wang G, Zhang G, Bai Z, Yang L. A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed. In Feng X, Bhattacharjya A, editors, International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023. SPIE. 2023. 126454N. (Proceedings of SPIE - The International Society for Optical Engineering). doi: 10.1117/12.2681299

A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this