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

School of Power and Energy

Northwestern Polytechnical University Xian

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

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.

Original language	English
Pages (from-to)	73-77
Number of pages	5
Journal	Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
Volume	29
Issue number	1
State	Published - Feb 2011

Keywords

Capture coefficient
Expansion in width
Inlet
Total pressure recovery

Cite this

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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",

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language = "英语",

volume = "29",

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

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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

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SN - 0258-1825

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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

Abstract

Keywords

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