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Universiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"

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dc.citedby2
dc.contributor.authorAmir A.-F.en_US
dc.contributor.authorYusaf T.en_US
dc.contributor.authorYusoff M.Z.en_US
dc.contributor.authorid15750212500en_US
dc.contributor.authorid23112065900en_US
dc.contributor.authorid7003976733en_US
dc.date.accessioned2023-12-28T08:57:50Z
dc.date.available2023-12-28T08:57:50Z
dc.date.issued2006
dc.description.abstractThe first phase of this paper is aimed to develop a standard test procedure for short-duration hypersonic test facility that build at the Universiti Tenaga Nasional "UNITEN" in Malaysia. The facility has been designed, built, and commissioned for different values of diaphragm pressure ratios. A theoretical model was developed to evaluate the Mach number values as a function of diaphragm pressure ratio for different working fluids. The second phase is to run experimental tests for different operating conditions. The calculated parameters which are pressure, temperature and velocity were very comparable to the practical results. A high precision in house made thermocouple was used to measure the temperature profile during the facility operation. A numerical transient heat transfer mathematical model was developed to evaluate the heat flux from the surface temperature history. The principle of operation and the reasoning behind building such a facility are explained, and the governing equations for the shock tube are presented. Copyright � 2006 by ASME.en_US
dc.description.natureFinalen_US
dc.identifier.scopus2-s2.0-33845782510
dc.identifier.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-33845782510&partnerID=40&md5=e65dcbf8a7dba6d5c647c9f9db958682
dc.identifier.urihttps://irepository.uniten.edu.my/handle/123456789/29834
dc.identifier.volume2006
dc.pagecount9
dc.sourceScopus
dc.sourcetitleProceedings of 8th Biennial ASME Conference on Engineering Systems Design and Analysis, ESDA2006
dc.subjectGun tunnel
dc.subjectMach number
dc.subjectShock tube
dc.subjectShock tunnel
dc.subjectShock wave
dc.subjectCalibration
dc.subjectDiaphragms
dc.subjectHeat flux
dc.subjectHeat transfer
dc.subjectMathematical models
dc.subjectShock tubes
dc.subjectShock waves
dc.subjectTest facilities
dc.subjectThermocouples
dc.subjectVelocity measurement
dc.subjectGun tunnels
dc.subjectHypersonic test facilities
dc.subjectMach number
dc.subjectShock tunnels
dc.subjectHypersonic aerodynamics
dc.titleUniversiti Tenaga Nasional short duration hypersonic test faciliy "calibration and verification"en_US
dc.typeConference paperen_US
dspace.entity.typePublication
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