Fast response surface temperature sensor for hypersonic vehicles 1

H. A. Mohammed, H. Salleh, M. Z. Yusoff

Research output: Contribution to journalArticle

6 Citations (Scopus)

Abstract

This 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 μs), and a rise time in studies of a transient surface temperature is less than 0.5 μs.

Original languageEnglish
Pages (from-to)153-159
Number of pages7
JournalInstruments and Experimental Techniques
Volume53
Issue number1
DOIs
Publication statusPublished - 01 Jan 2010

Fingerprint

hypersonic vehicles
Hypersonic vehicles
temperature sensors
Temperature sensors
surface temperature
constantan
Shock tubes
shock tubes
heat transfer
Calibration
Heat transfer
Fabrication
Temperature
fabrication
evaluation

All Science Journal Classification (ASJC) codes

  • Instrumentation

Cite this

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Fast response surface temperature sensor for hypersonic vehicles 1. / Mohammed, H. A.; Salleh, H.; Yusoff, M. Z.

In: Instruments and Experimental Techniques, Vol. 53, No. 1, 01.01.2010, p. 153-159.

Research output: Contribution to journalArticle

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