NDLI: Application of fluorescence pressure transducer technology to pressure measurement test in high speed wind tunnel

Content Provider	IEEE Xplore Digital Library
Author	Chen XueYuan
Copyright Year	2012
Description	Author affiliation: AVIC Aerodynamics Research Institute, Shenyang, 110034, China (Chen XueYuan)
Abstract	Pressure measurement has always been an important part of aircraft wind tunnel tests. The traditional method of pressure measurement uses the model with a series of special pressure taps on its surface to get discontinuous pressure data. Recently, Pressure Sensitive Paint (PSP) technology which uses optical method for measuring pressure distribution of the surface of the specific area has attracted much attention as an effective approach for pressure measurement. This paper introduces the basic theory of the Pressure Sensitive Paint (PSP) measurement technology and the development of control system for the experiments. The analysis of the experiments data provides the credible evidence for the farther popularization of the Pressure Sensitive Paint (PSP) measurement technology.
Starting Page	1221
Ending Page	1225
File Size	1165100
Page Count	5
File Format	PDF
ISBN	9781457720734
e-ISBN	9781457720741
DOI	10.1109/CCDC.2012.6242997
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2012-05-23
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Charge coupled devices Pressure Sensitive Paint Digital CCD Camera Fluorescence Optical variables measurement Calibration Pressure measurement Experiments Control Optical sensors Mathematical model Optical Pressure Measurement
Content Type	Text
Resource Type	Article

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4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
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