An aerodynamic characteristics analysis for miniature transonic compressors of aero-engines with quasi-three dimensional calculation program of S2 stream surface

Ning Yuan; Zhenjia Zhang; Zhonghua Gu; Guotai Feng

An aerodynamic characteristics analysis for miniature transonic compressors of aero-engines with quasi-three dimensional calculation program of S₂ stream surface

Ning Yuan^*
, Zhenjia Zhang
, Zhonghua Gu
, Guotai Feng

^*Corresponding author for this work

School of Energy Science and Engineering

CASIC
Harbin Institute of Technology

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

2 Scopus citations

Abstract

In the this paper, Quasi-Three Dimensional calculation program of S₂ stream surface is applied to analyze aerodynamic characteristics for two typical miniature transonic compressors of Aero-engines (model I and model I ) . The internal flow situation and improvement methods are discussed. The authors expert to provide some thinking and illuminating remarks for improvement of this kind of compressors.

Original language	English
Pages (from-to)	33+63
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	17
Issue number	6
State	Published - 1996

Keywords

Aerodynamic characteristics
Nemerical calculation
Transonic compressor
Turbojet engine

Cite this

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title = "An aerodynamic characteristics analysis for miniature transonic compressors of aero-engines with quasi-three dimensional calculation program of S2 stream surface",

abstract = "In the this paper, Quasi-Three Dimensional calculation program of S2 stream surface is applied to analyze aerodynamic characteristics for two typical miniature transonic compressors of Aero-engines (model I and model I ) . The internal flow situation and improvement methods are discussed. The authors expert to provide some thinking and illuminating remarks for improvement of this kind of compressors.",

keywords = "Aerodynamic characteristics, Nemerical calculation, Transonic compressor, Turbojet engine",

author = "Ning Yuan and Zhenjia Zhang and Zhonghua Gu and Guotai Feng",

year = "1996",

language = "英语",

volume = "17",

pages = "33+63",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

number = "6",

}

TY - JOUR

T1 - An aerodynamic characteristics analysis for miniature transonic compressors of aero-engines with quasi-three dimensional calculation program of S2 stream surface

AU - Yuan, Ning

AU - Zhang, Zhenjia

AU - Gu, Zhonghua

AU - Feng, Guotai

PY - 1996

Y1 - 1996

N2 - In the this paper, Quasi-Three Dimensional calculation program of S2 stream surface is applied to analyze aerodynamic characteristics for two typical miniature transonic compressors of Aero-engines (model I and model I ) . The internal flow situation and improvement methods are discussed. The authors expert to provide some thinking and illuminating remarks for improvement of this kind of compressors.

AB - In the this paper, Quasi-Three Dimensional calculation program of S2 stream surface is applied to analyze aerodynamic characteristics for two typical miniature transonic compressors of Aero-engines (model I and model I ) . The internal flow situation and improvement methods are discussed. The authors expert to provide some thinking and illuminating remarks for improvement of this kind of compressors.

KW - Aerodynamic characteristics

KW - Nemerical calculation

KW - Transonic compressor

KW - Turbojet engine

UR - https://www.scopus.com/pages/publications/4243185031

M3 - 文章

AN - SCOPUS:4243185031

SN - 1001-4055

VL - 17

SP - 33+63

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 6

ER -

An aerodynamic characteristics analysis for miniature transonic compressors of aero-engines with quasi-three dimensional calculation program of S₂ stream surface

Abstract

Keywords

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