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Fast response surface temperature sensor for hypersonic vehicles 1

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dc.citedby15
dc.contributor.authorMohammed H.A.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.accessioned2023-12-29T07:51:31Z
dc.date.available2023-12-29T07:51:31Z
dc.date.issued2010
dc.description.abstractThis paper describes the design, fabrication, and evaluation technique of fast response Surface Temperature Sensor (STS). This STS was made of chromel-constantan elements with 2.2 and 0.8 mm in diameter. The calibration technique using shock tube facility for measuring the transient surface temperature and heat transfer rate is also presented. It has been proved that the STS response time is very short (less than 50 ?s), and a rise time in studies of a transient surface temperature is less than 0.5 ?s. � 2010 Pleiades Publishing, Ltd.en_US
dc.description.natureFinalen_US
dc.identifier.doi10.1134/S0020441210010288
dc.identifier.epage159
dc.identifier.issue1
dc.identifier.scopus2-s2.0-77950825761
dc.identifier.spage153
dc.identifier.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-77950825761&doi=10.1134%2fS0020441210010288&partnerID=40&md5=e41658f36f6262c40872f537e6d63681
dc.identifier.urihttps://irepository.uniten.edu.my/handle/123456789/30699
dc.identifier.volume53
dc.pagecount6
dc.sourceScopus
dc.sourcetitleInstruments and Experimental Techniques
dc.subjectAtmospheric temperature
dc.subjectHypersonic aerodynamics
dc.subjectHypersonic vehicles
dc.subjectTemperature sensors
dc.subjectCalibration techniques
dc.subjectFast response
dc.subjectHeat transfer rate
dc.subjectResponse time
dc.subjectRisetimes
dc.subjectShock tube facility
dc.subjectSurface temperatures
dc.subjectSurface properties
dc.titleFast response surface temperature sensor for hypersonic vehicles 1en_US
dc.typeArticleen_US
dspace.entity.typePublication
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