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

^*此作品的通讯作者

能源与动力工程学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

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.

源语言	英语
页（从-至）	1752-1758
页数	7
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	24
期	8
出版状态	已出版 - 8月 2009

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引用此

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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",

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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

摘要

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