Publication:
Calibration of rugged, renewable and fast response temperature probes in a hypersonic flow facility

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dc.citedby0
dc.contributor.authorMohammed H.en_US
dc.contributor.authorSalleh H.en_US
dc.contributor.authorYusoff M.Z.en_US
dc.contributor.authorid15837504600en_US
dc.contributor.authorid24067645400en_US
dc.contributor.authorid7003976733en_US
dc.date.accessioned2023-12-29T07:51:08Z
dc.date.available2023-12-29T07:51:08Z
dc.date.issued2010
dc.description.abstractThis paper presents a dynamic calibration technique of rugged, renewable and fast response temperature probes (TP) in a hypersonic testing facility. Two types of scratch were used, mainly abrasive papers with different grit sizes and scalpel blades with different thicknesses to form the probe junction. The effect of scratch technique on probe's thermal product is investigated. The probes were tested and calibrated in the test section and in the end wall of UNITEN shock tube facility at different axial and radial locations. It was observed that the thermal product of a particular TP depends on the Mach number, surface junction scratch technique, junction location as well as on the enthalpy conditions. It was also noticed that using scalpel blade technique with a particular blade size gives consistent thermal product values. Thus, it does not require an individual calibration. However, for TP whose junction created using abrasive paper technique with different grit sizes, a calibration for each TP is likely to be needed. The results from shock tube tests have shown that, these probes have a response time on the order of microseconds (50 us) with a rise time less than (0.5 us), and were suitable for making the heat transfer measurements in highly transient conditions. Copyright � 2010 by ASME.en_US
dc.description.natureFinalen_US
dc.identifier.doi10.1115/IMECE2009-10925
dc.identifier.epage1060
dc.identifier.issuePART B
dc.identifier.scopus2-s2.0-77954294177
dc.identifier.spage1049
dc.identifier.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-77954294177&doi=10.1115%2fIMECE2009-10925&partnerID=40&md5=57ad496548294fba6b40a7cacc56b37d
dc.identifier.urihttps://irepository.uniten.edu.my/handle/123456789/30671
dc.identifier.volume9
dc.pagecount11
dc.publisherAmerican Society of Mechanical Engineers (ASME)en_US
dc.sourceScopus
dc.sourcetitleASME International Mechanical Engineering Congress and Exposition, Proceedings
dc.subjectAbrasives
dc.subjectCalibration
dc.subjectDynamic response
dc.subjectFacilities
dc.subjectLocation
dc.subjectMach number
dc.subjectMechanical engineering
dc.subjectShock tubes
dc.subjectDynamic calibration
dc.subjectEnd-wall
dc.subjectFast response
dc.subjectGrit size
dc.subjectHeat transfer measurements
dc.subjectRadial locations
dc.subjectResponse time
dc.subjectRisetimes
dc.subjectShock tube facility
dc.subjectSurface junctions
dc.subjectTemperature probes
dc.subjectTest sections
dc.subjectTesting facility
dc.subjectThermal products
dc.subjectTransient conditions
dc.subjectProbes
dc.titleCalibration of rugged, renewable and fast response temperature probes in a hypersonic flow facilityen_US
dc.typeConference Paperen_US
dspace.entity.typePublication
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