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

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This 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.

Original languageEnglish
Title of host publicationProceedings of the ASME International Mechanical Engineering Congress and Exposition 2009, IMECE 2009
PublisherAmerican Society of Mechanical Engineers (ASME)
Pages1049-1060
Number of pages12
Volume9
EditionPART B
ISBN (Print)9780791843826
DOIs
Publication statusPublished - 2010
EventASME 2009 International Mechanical Engineering Congress and Exposition, IMECE2009 - Lake Buena Vista, FL, United States
Duration: 13 Nov 200919 Nov 2009

Other

OtherASME 2009 International Mechanical Engineering Congress and Exposition, IMECE2009
CountryUnited States
CityLake Buena Vista, FL
Period13/11/0919/11/09

Fingerprint

Hypersonic flow
Calibration
Temperature
Shock tubes
Abrasives
Hypersonic aerodynamics
Mach number
Enthalpy
Heat transfer
Testing

All Science Journal Classification (ASJC) codes

  • Mechanical Engineering

Cite this

Mohammed, H., Salleh, H., & Yusoff, M. Z. (2010). Calibration of rugged, renewable and fast response temperature probes in a hypersonic flow facility. In Proceedings of the ASME International Mechanical Engineering Congress and Exposition 2009, IMECE 2009 (PART B ed., Vol. 9, pp. 1049-1060). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/IMECE2009-10925
Mohammed, H. ; Salleh, Hanim ; Yusoff, Mohd Zamri. / Calibration of rugged, renewable and fast response temperature probes in a hypersonic flow facility. Proceedings of the ASME International Mechanical Engineering Congress and Exposition 2009, IMECE 2009. Vol. 9 PART B. ed. American Society of Mechanical Engineers (ASME), 2010. pp. 1049-1060
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Mohammed, H, Salleh, H & Yusoff, MZ 2010, Calibration of rugged, renewable and fast response temperature probes in a hypersonic flow facility. in Proceedings of the ASME International Mechanical Engineering Congress and Exposition 2009, IMECE 2009. PART B edn, vol. 9, American Society of Mechanical Engineers (ASME), pp. 1049-1060, ASME 2009 International Mechanical Engineering Congress and Exposition, IMECE2009, Lake Buena Vista, FL, United States, 13/11/09. https://doi.org/10.1115/IMECE2009-10925

Calibration of rugged, renewable and fast response temperature probes in a hypersonic flow facility. / Mohammed, H.; Salleh, Hanim; Yusoff, Mohd Zamri.

Proceedings of the ASME International Mechanical Engineering Congress and Exposition 2009, IMECE 2009. Vol. 9 PART B. ed. American Society of Mechanical Engineers (ASME), 2010. p. 1049-1060.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Mohammed H, Salleh H, Yusoff MZ. Calibration of rugged, renewable and fast response temperature probes in a hypersonic flow facility. In Proceedings of the ASME International Mechanical Engineering Congress and Exposition 2009, IMECE 2009. PART B ed. Vol. 9. American Society of Mechanical Engineers (ASME). 2010. p. 1049-1060 https://doi.org/10.1115/IMECE2009-10925