The effects of steady circumferential combined distortion on characteristics and flow field of compressor

Wenyan Song; Zhanxue Wang; Diyi Tang

The effects of steady circumferential combined distortion on characteristics and flow field of compressor

Wenyan Song
, Zhanxue Wang
, Diyi Tang

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

The radial-equilibrium equation and multi-sector parallel compressor model are used to settle complex distorted flow field in this paper. The effects of inlet flow field combined distortion on compressor characteristics and performance are calculated. The details of compressor flow field with inlet distortion are described.

源语言	英语
页（从-至）	82-86
页数	5
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	18
期	5
出版状态	已出版 - 1997

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title = "The effects of steady circumferential combined distortion on characteristics and flow field of compressor",

abstract = "The radial-equilibrium equation and multi-sector parallel compressor model are used to settle complex distorted flow field in this paper. The effects of inlet flow field combined distortion on compressor characteristics and performance are calculated. The details of compressor flow field with inlet distortion are described.",

keywords = "Axial flow compressor, Flow distortion, Numerical calculation",

author = "Wenyan Song and Zhanxue Wang and Diyi Tang",

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T1 - The effects of steady circumferential combined distortion on characteristics and flow field of compressor

AU - Song, Wenyan

AU - Wang, Zhanxue

AU - Tang, Diyi

PY - 1997

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N2 - The radial-equilibrium equation and multi-sector parallel compressor model are used to settle complex distorted flow field in this paper. The effects of inlet flow field combined distortion on compressor characteristics and performance are calculated. The details of compressor flow field with inlet distortion are described.

AB - The radial-equilibrium equation and multi-sector parallel compressor model are used to settle complex distorted flow field in this paper. The effects of inlet flow field combined distortion on compressor characteristics and performance are calculated. The details of compressor flow field with inlet distortion are described.

KW - Axial flow compressor

KW - Flow distortion

KW - Numerical calculation

UR - https://www.scopus.com/pages/publications/0031363472

M3 - 文章

AN - SCOPUS:0031363472

SN - 1001-4055

VL - 18

SP - 82

EP - 86

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 5

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The effects of steady circumferential combined distortion on characteristics and flow field of compressor

摘要

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