Design and experimental study of the inlet temperature distortion generator

Min Jie Hou; Da Xiang Liu; Hui Ru Wang

Design and experimental study of the inlet temperature distortion generator

Min Jie Hou^*
, Da Xiang Liu
, Hui Ru Wang

^*此作品的通讯作者

材料科学与工程学院

科研成果: 期刊稿件 › 文章 › 同行评审

5 引用（Scopus）

摘要

The Temperature Distortion Generator (TDG) design specifications, design technique and the technology of its fabrication were presented. The TDG was tested and calibrated using a turbojet engine and a turbofan engine. The test results indicate that the specifications of this TDG satisfy the requirements of engine temperature distortion testing. The equipment is highly reliable, controllable and stable.

源语言	英语
页（从-至）	361-367
页数	7
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	20
期	3
出版状态	已出版 - 6月 2005

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引用此

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title = "Design and experimental study of the inlet temperature distortion generator",

abstract = "The Temperature Distortion Generator (TDG) design specifications, design technique and the technology of its fabrication were presented. The TDG was tested and calibrated using a turbojet engine and a turbofan engine. The test results indicate that the specifications of this TDG satisfy the requirements of engine temperature distortion testing. The equipment is highly reliable, controllable and stable.",

keywords = "Aerodynamic stability, Aerospace propulsion system, Temperature distortion, Temperature distortion generator, Turbofan, Turbojet",

author = "Hou, \{Min Jie\} and Liu, \{Da Xiang\} and Wang, \{Hui Ru\}",

year = "2005",

month = jun,

language = "英语",

volume = "20",

pages = "361--367",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

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number = "3",

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T1 - Design and experimental study of the inlet temperature distortion generator

AU - Hou, Min Jie

AU - Liu, Da Xiang

AU - Wang, Hui Ru

PY - 2005/6

Y1 - 2005/6

N2 - The Temperature Distortion Generator (TDG) design specifications, design technique and the technology of its fabrication were presented. The TDG was tested and calibrated using a turbojet engine and a turbofan engine. The test results indicate that the specifications of this TDG satisfy the requirements of engine temperature distortion testing. The equipment is highly reliable, controllable and stable.

AB - The Temperature Distortion Generator (TDG) design specifications, design technique and the technology of its fabrication were presented. The TDG was tested and calibrated using a turbojet engine and a turbofan engine. The test results indicate that the specifications of this TDG satisfy the requirements of engine temperature distortion testing. The equipment is highly reliable, controllable and stable.

KW - Aerodynamic stability

KW - Aerospace propulsion system

KW - Temperature distortion

KW - Temperature distortion generator

KW - Turbofan

KW - Turbojet

UR - https://www.scopus.com/pages/publications/22844434166

M3 - 文章

AN - SCOPUS:22844434166

SN - 1000-8055

VL - 20

SP - 361

EP - 367

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 3

ER -

Design and experimental study of the inlet temperature distortion generator

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