Numerical simulation of two dimension iced airfoil using immersed boundary method

Guo Hua Zhong; Xiao Feng Sun

Numerical simulation of two dimension iced airfoil using immersed boundary method

Guo Hua Zhong^*
, Xiao Feng Sun

^*Corresponding author for this work

School of Energy and Power Engineering

Beihang University

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

Abstract

An immersed boundary method was applied to numerical simulation of the flow past a clean/iced NACA0012 airfoil. In this paper, two dimension imcompressible Reynolds-averaged Navier-Stokes equations were solved with SIMPLEC method. One equation turbulence model-Spalart-Allmaras turbulence model, was used in the numerical procedure. Good agreement was found between the present numerical results and previous experimental work.

Original language	English
Pages (from-to)	1752-1758
Number of pages	7
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	24
Issue number	8
State	Published - Aug 2009

Keywords

Iced airfoil
Immersed boundary method
Spalart-Allmaras turbulence model

Cite this

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title = "Numerical simulation of two dimension iced airfoil using immersed boundary method",

abstract = "An immersed boundary method was applied to numerical simulation of the flow past a clean/iced NACA0012 airfoil. In this paper, two dimension imcompressible Reynolds-averaged Navier-Stokes equations were solved with SIMPLEC method. One equation turbulence model-Spalart-Allmaras turbulence model, was used in the numerical procedure. Good agreement was found between the present numerical results and previous experimental work.",

keywords = "Iced airfoil, Immersed boundary method, Spalart-Allmaras turbulence model",

author = "Zhong, \{Guo Hua\} and Sun, \{Xiao Feng\}",

year = "2009",

month = aug,

language = "英语",

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journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

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T1 - Numerical simulation of two dimension iced airfoil using immersed boundary method

AU - Zhong, Guo Hua

AU - Sun, Xiao Feng

PY - 2009/8

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N2 - An immersed boundary method was applied to numerical simulation of the flow past a clean/iced NACA0012 airfoil. In this paper, two dimension imcompressible Reynolds-averaged Navier-Stokes equations were solved with SIMPLEC method. One equation turbulence model-Spalart-Allmaras turbulence model, was used in the numerical procedure. Good agreement was found between the present numerical results and previous experimental work.

AB - An immersed boundary method was applied to numerical simulation of the flow past a clean/iced NACA0012 airfoil. In this paper, two dimension imcompressible Reynolds-averaged Navier-Stokes equations were solved with SIMPLEC method. One equation turbulence model-Spalart-Allmaras turbulence model, was used in the numerical procedure. Good agreement was found between the present numerical results and previous experimental work.

KW - Iced airfoil

KW - Immersed boundary method

KW - Spalart-Allmaras turbulence model

UR - https://www.scopus.com/pages/publications/69749112951

M3 - 文章

AN - SCOPUS:69749112951

SN - 1000-8055

VL - 24

SP - 1752

EP - 1758

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 8

ER -

Numerical simulation of two dimension iced airfoil using immersed boundary method

Abstract

Keywords

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