Determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow

This paper presents an experimental method for determining the effusivity values of different scratched coaxial temperature sensors. These sensors have a response time on the order of microseconds (50 ?s) with a rise time of less than 0.3 ?s. Two types of scratch were used, mainly abrasive papers wi...

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Main Authors: Mohammed H.A., Salleh H., Yusoff M.Z.
Other Authors: 15837504600
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Published: 2023
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spelling my.uniten.dspace-305522023-12-29T15:49:21Z Determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow Mohammed H.A. Salleh H. Yusoff M.Z. 15837504600 24067645400 7003976733 Coaxial temperature sensors Effusivity Scratched technique Shock tube Transient heat flux Abrasives Calibration Mach number Shock tubes Temperature sensors Coaxial temperature sensors Effusivity Experimental methods Grit size Individual calibrations Operating condition Response time Risetimes Scratched technique Test sections Transient heat flux Transient heat transfer Heat flux This paper presents an experimental method for determining the effusivity values of different scratched coaxial temperature sensors. These sensors have a response time on the order of microseconds (50 ?s) with a rise time of less than 0.3 ?s. Two types of scratch were used, mainly abrasive papers with different grit sizes and scalpel blades with different thicknesses to form the sensor junctions. The effect of the scratch technique on the sensor's effusivity is also investigated. The sensors were tested and calibrated in the test section of a shock-tube facility at different operating conditions. It was observed that the effusivity of a particular sensor depends on the Mach number, scratch technique, scratch direction, junction location, as well as on the enthalpy condition. It was also noticed that a scratched sensor using the scalpel blade technique does not require an individual calibration. However, for a sensor scratched using the abrasive paper technique, a calibration for each sensor is likely to be required. The present results have provided useful and practical data of the effusivity values for different scratched temperature sensors. These data are beneficial to experimentalists in the field, and can be used for accurate transient heat transfer rate measurements. � 2010 Springer Science+Business Media, LLC. Final 2023-12-29T07:49:20Z 2023-12-29T07:49:20Z 2010 Article 10.1007/s10765-010-0882-x 2-s2.0-78650873395 https://www.scopus.com/inward/record.uri?eid=2-s2.0-78650873395&doi=10.1007%2fs10765-010-0882-x&partnerID=40&md5=1d2aa7db8d91db69cdf84194ecf0d818 https://irepository.uniten.edu.my/handle/123456789/30552 31 11/12/2023 2305 2322 Scopus
institution Universiti Tenaga Nasional
building UNITEN Library
collection Institutional Repository
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country Malaysia
content_provider Universiti Tenaga Nasional
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topic Coaxial temperature sensors
Effusivity
Scratched technique
Shock tube
Transient heat flux
Abrasives
Calibration
Mach number
Shock tubes
Temperature sensors
Coaxial temperature sensors
Effusivity
Experimental methods
Grit size
Individual calibrations
Operating condition
Response time
Risetimes
Scratched technique
Test sections
Transient heat flux
Transient heat transfer
Heat flux
spellingShingle Coaxial temperature sensors
Effusivity
Scratched technique
Shock tube
Transient heat flux
Abrasives
Calibration
Mach number
Shock tubes
Temperature sensors
Coaxial temperature sensors
Effusivity
Experimental methods
Grit size
Individual calibrations
Operating condition
Response time
Risetimes
Scratched technique
Test sections
Transient heat flux
Transient heat transfer
Heat flux
Mohammed H.A.
Salleh H.
Yusoff M.Z.
Determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow
description This paper presents an experimental method for determining the effusivity values of different scratched coaxial temperature sensors. These sensors have a response time on the order of microseconds (50 ?s) with a rise time of less than 0.3 ?s. Two types of scratch were used, mainly abrasive papers with different grit sizes and scalpel blades with different thicknesses to form the sensor junctions. The effect of the scratch technique on the sensor's effusivity is also investigated. The sensors were tested and calibrated in the test section of a shock-tube facility at different operating conditions. It was observed that the effusivity of a particular sensor depends on the Mach number, scratch technique, scratch direction, junction location, as well as on the enthalpy condition. It was also noticed that a scratched sensor using the scalpel blade technique does not require an individual calibration. However, for a sensor scratched using the abrasive paper technique, a calibration for each sensor is likely to be required. The present results have provided useful and practical data of the effusivity values for different scratched temperature sensors. These data are beneficial to experimentalists in the field, and can be used for accurate transient heat transfer rate measurements. � 2010 Springer Science+Business Media, LLC.
author2 15837504600
author_facet 15837504600
Mohammed H.A.
Salleh H.
Yusoff M.Z.
format Article
author Mohammed H.A.
Salleh H.
Yusoff M.Z.
author_sort Mohammed H.A.
title Determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow
title_short Determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow
title_full Determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow
title_fullStr Determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow
title_full_unstemmed Determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow
title_sort determination of the effusivity of different scratched coaxial temperature sensors under hypersonic flow
publishDate 2023
_version_ 1806427549657464832
score 13.188404