Characteristic analysis of supersonic 2D inlet flow field

Jian Dong Zhang; Zhan Xue Wang; Zeng Wen Liu; Yuan Hu Cai; Chun Yang Liu

Characteristic analysis of supersonic 2D inlet flow field

Jian Dong Zhang, Zhan Xue Wang, Zeng Wen Liu, Yuan Hu Cai, Chun Yang Liu

动力与能源学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

In order to analyse the performance of supersonic inlet, one-dimensional aerodynamic analysis and three-dimensional numerical simulation are used. The results show that expansion in width cannot be neglected. Expansion in width can lead to the increase of inlet throat Mach number, which results in the decrease of inlet total pressure recovery and flow capture efficient.

源语言	英语
页（从-至）	73-77
页数	5
期刊	Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
卷	29
期	1
出版状态	已出版 - 2月 2011

其它文件与链接

链接到 Scopus 的出版物

引用此

@article{65ac8a24f3aa44d6814725a7ba559a66,

title = "Characteristic analysis of supersonic 2D inlet flow field",

abstract = "In order to analyse the performance of supersonic inlet, one-dimensional aerodynamic analysis and three-dimensional numerical simulation are used. The results show that expansion in width cannot be neglected. Expansion in width can lead to the increase of inlet throat Mach number, which results in the decrease of inlet total pressure recovery and flow capture efficient.",

keywords = "Capture coefficient, Expansion in width, Inlet, Total pressure recovery",

author = "Zhang, {Jian Dong} and Wang, {Zhan Xue} and Liu, {Zeng Wen} and Cai, {Yuan Hu} and Liu, {Chun Yang}",

year = "2011",

month = feb,

language = "英语",

volume = "29",

pages = "73--77",

journal = "Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica",

issn = "0258-1825",

publisher = "Zhongguo Kongqi Dongli Yanjiu yu Fazhan Zhongxin",

number = "1",

}

TY - JOUR

T1 - Characteristic analysis of supersonic 2D inlet flow field

AU - Zhang, Jian Dong

AU - Wang, Zhan Xue

AU - Liu, Zeng Wen

AU - Cai, Yuan Hu

AU - Liu, Chun Yang

PY - 2011/2

Y1 - 2011/2

N2 - In order to analyse the performance of supersonic inlet, one-dimensional aerodynamic analysis and three-dimensional numerical simulation are used. The results show that expansion in width cannot be neglected. Expansion in width can lead to the increase of inlet throat Mach number, which results in the decrease of inlet total pressure recovery and flow capture efficient.

AB - In order to analyse the performance of supersonic inlet, one-dimensional aerodynamic analysis and three-dimensional numerical simulation are used. The results show that expansion in width cannot be neglected. Expansion in width can lead to the increase of inlet throat Mach number, which results in the decrease of inlet total pressure recovery and flow capture efficient.

KW - Capture coefficient

KW - Expansion in width

KW - Inlet

KW - Total pressure recovery

UR - http://www.scopus.com/inward/record.url?scp=79953736219&partnerID=8YFLogxK

M3 - 文章

AN - SCOPUS:79953736219

SN - 0258-1825

VL - 29

SP - 73

EP - 77

JO - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

JF - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

IS - 1

ER -

Characteristic analysis of supersonic 2D inlet flow field

摘要

其它文件与链接

指纹

引用此