Effect of inlet pressure distortion on stability margin of missile turbojet engine

Xinnong Ye; Zhanxue Wang; Weiyang Qiao

Effect of inlet pressure distortion on stability margin of missile turbojet engine

Xinnong Ye
, Zhanxue Wang
, Weiyang Qiao

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

2 引用（Scopus）

摘要

The surge of missile turbojet engine is disastrous for the missile, so it is important to ensure its stability margin. The pressure distortion of the inlet of turbojet engine has an important effect on its stability margin. According to the model of parallel compressor and Liapunov theory, a program for computing the effect of inlet pressure distortion on the surge and running line of missile turbojet engine is developed. A numerical example is given to illustrate the loss of surge margin.

源语言	英语
页（从-至）	266-268
页数	3
期刊	Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University
卷	21
期	3
出版状态	已出版 - 6月 2003

其它文件与链接

链接到 Scopus 的出版物

引用此

@article{0a64e85f599743ec9d85435b5c8190b8,

title = "Effect of inlet pressure distortion on stability margin of missile turbojet engine",

abstract = "The surge of missile turbojet engine is disastrous for the missile, so it is important to ensure its stability margin. The pressure distortion of the inlet of turbojet engine has an important effect on its stability margin. According to the model of parallel compressor and Liapunov theory, a program for computing the effect of inlet pressure distortion on the surge and running line of missile turbojet engine is developed. A numerical example is given to illustrate the loss of surge margin.",

keywords = "Inlet pressure distortion, Missile turbojet engine, Stability margin, Surge",

author = "Xinnong Ye and Zhanxue Wang and Weiyang Qiao",

year = "2003",

month = jun,

language = "英语",

volume = "21",

pages = "266--268",

journal = "Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University",

issn = "1000-2758",

publisher = "Northwestern Polytechnical University",

number = "3",

}

TY - JOUR

T1 - Effect of inlet pressure distortion on stability margin of missile turbojet engine

AU - Ye, Xinnong

AU - Wang, Zhanxue

AU - Qiao, Weiyang

PY - 2003/6

Y1 - 2003/6

N2 - The surge of missile turbojet engine is disastrous for the missile, so it is important to ensure its stability margin. The pressure distortion of the inlet of turbojet engine has an important effect on its stability margin. According to the model of parallel compressor and Liapunov theory, a program for computing the effect of inlet pressure distortion on the surge and running line of missile turbojet engine is developed. A numerical example is given to illustrate the loss of surge margin.

AB - The surge of missile turbojet engine is disastrous for the missile, so it is important to ensure its stability margin. The pressure distortion of the inlet of turbojet engine has an important effect on its stability margin. According to the model of parallel compressor and Liapunov theory, a program for computing the effect of inlet pressure distortion on the surge and running line of missile turbojet engine is developed. A numerical example is given to illustrate the loss of surge margin.

KW - Inlet pressure distortion

KW - Missile turbojet engine

KW - Stability margin

KW - Surge

UR - https://www.scopus.com/pages/publications/0141508871

M3 - 文章

AN - SCOPUS:0141508871

SN - 1000-2758

VL - 21

SP - 266

EP - 268

JO - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

JF - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

IS - 3

ER -

Effect of inlet pressure distortion on stability margin of missile turbojet engine

摘要

其它文件与链接

学术指纹

引用此