Direct measurement system of pressure distribution on airfoil surface using micro pressure sensor array

Ying Chang; Bing He Ma; Jin Jun Deng; Shuang Chen; Wei Zheng Yuan

Direct measurement system of pressure distribution on airfoil surface using micro pressure sensor array

Ying Chang
, Bing He Ma
, Jin Jun Deng
, Shuang Chen
, Wei Zheng Yuan

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

2 引用（Scopus）

摘要

A system based on a micro pressure sensor array was designed and established to measure pressure distribution of airfoil surface. Assembled onto a flexible polyimide substrate, the sensor array can be mounted upon airfoil surface easily. Related wind tunnel experiments were carried out. It shows this system can accomplish on-line measurement, real-time data processing and display, and has potential of dynamic pressure measurement of flow around non-planar surface. Measurement results with such system are coincident with those obtained through conventional pressure scan valve.

源语言	英语
页（从-至）	89-93
页数	5
期刊	Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics
卷	22
期	3
出版状态	已出版 - 9月 2008

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引用此

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abstract = "A system based on a micro pressure sensor array was designed and established to measure pressure distribution of airfoil surface. Assembled onto a flexible polyimide substrate, the sensor array can be mounted upon airfoil surface easily. Related wind tunnel experiments were carried out. It shows this system can accomplish on-line measurement, real-time data processing and display, and has potential of dynamic pressure measurement of flow around non-planar surface. Measurement results with such system are coincident with those obtained through conventional pressure scan valve.",

keywords = "Airfoil surface, Flexible polyimide substrate, Micro pressure sensor array, Pressure distribution, Real-time measurement",

author = "Ying Chang and Ma, \{Bing He\} and Deng, \{Jin Jun\} and Shuang Chen and Yuan, \{Wei Zheng\}",

year = "2008",

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language = "英语",

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T1 - Direct measurement system of pressure distribution on airfoil surface using micro pressure sensor array

AU - Chang, Ying

AU - Ma, Bing He

AU - Deng, Jin Jun

AU - Chen, Shuang

AU - Yuan, Wei Zheng

PY - 2008/9

Y1 - 2008/9

N2 - A system based on a micro pressure sensor array was designed and established to measure pressure distribution of airfoil surface. Assembled onto a flexible polyimide substrate, the sensor array can be mounted upon airfoil surface easily. Related wind tunnel experiments were carried out. It shows this system can accomplish on-line measurement, real-time data processing and display, and has potential of dynamic pressure measurement of flow around non-planar surface. Measurement results with such system are coincident with those obtained through conventional pressure scan valve.

AB - A system based on a micro pressure sensor array was designed and established to measure pressure distribution of airfoil surface. Assembled onto a flexible polyimide substrate, the sensor array can be mounted upon airfoil surface easily. Related wind tunnel experiments were carried out. It shows this system can accomplish on-line measurement, real-time data processing and display, and has potential of dynamic pressure measurement of flow around non-planar surface. Measurement results with such system are coincident with those obtained through conventional pressure scan valve.

KW - Airfoil surface

KW - Flexible polyimide substrate

KW - Micro pressure sensor array

KW - Pressure distribution

KW - Real-time measurement

UR - https://www.scopus.com/pages/publications/55149100691

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EP - 93

JO - Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics

JF - Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics

IS - 3

ER -

Direct measurement system of pressure distribution on airfoil surface using micro pressure sensor array

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