Three-points NURBS parameterized method for compressor intermediate duct

Xiao Ming Deng; Li Min Gao; Xu Dong Feng; Bo Liu

Three-points NURBS parameterized method for compressor intermediate duct

Xiao Ming Deng, Li Min Gao, Xu Dong Feng, Bo Liu

动力与能源学院

科研成果: 期刊稿件 › 文章 › 同行评审

2 引用（Scopus）

摘要

A fast and efficient parameterized method for the compressor intermediate duct is explored, in order to determine the initial geometry with good aerodynamic performance for the 3D optimization. Results validate: endwall lines of 2D initial design generated by the three-points NURBS curve parameterized method agree with 3D optimized result very well and are able to predict the flow loss of compressor intermediate duct accurately.

源语言	英语
页（从-至）	1330-1333
页数	4
期刊	Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
卷	35
期	7
出版状态	已出版 - 7月 2014

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链接到 Scopus 的出版物

引用此

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title = "Three-points NURBS parameterized method for compressor intermediate duct",

abstract = "A fast and efficient parameterized method for the compressor intermediate duct is explored, in order to determine the initial geometry with good aerodynamic performance for the 3D optimization. Results validate: endwall lines of 2D initial design generated by the three-points NURBS curve parameterized method agree with 3D optimized result very well and are able to predict the flow loss of compressor intermediate duct accurately.",

keywords = "Compressor intermediate duct, Initial design, Parameterized method",

author = "Deng, {Xiao Ming} and Gao, {Li Min} and Feng, {Xu Dong} and Bo Liu",

year = "2014",

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volume = "35",

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AU - Deng, Xiao Ming

AU - Gao, Li Min

AU - Feng, Xu Dong

AU - Liu, Bo

PY - 2014/7

Y1 - 2014/7

N2 - A fast and efficient parameterized method for the compressor intermediate duct is explored, in order to determine the initial geometry with good aerodynamic performance for the 3D optimization. Results validate: endwall lines of 2D initial design generated by the three-points NURBS curve parameterized method agree with 3D optimized result very well and are able to predict the flow loss of compressor intermediate duct accurately.

AB - A fast and efficient parameterized method for the compressor intermediate duct is explored, in order to determine the initial geometry with good aerodynamic performance for the 3D optimization. Results validate: endwall lines of 2D initial design generated by the three-points NURBS curve parameterized method agree with 3D optimized result very well and are able to predict the flow loss of compressor intermediate duct accurately.

KW - Compressor intermediate duct

KW - Initial design

KW - Parameterized method

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M3 - 文章

AN - SCOPUS:84904883162

SN - 0253-231X

VL - 35

SP - 1330

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JO - Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics

JF - Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics

IS - 7

ER -

Three-points NURBS parameterized method for compressor intermediate duct

摘要

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