Fast response surface temperature sensor for hypersonic vehicles 1

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

doi:10.1134/S0020441210010288

Fast response surface temperature sensor for hypersonic vehicles ¹

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

Department of Mechanical Engineering

Research output: Contribution to journal › Article

7 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 language	English
Pages (from-to)	153-159
Number of pages	7
Journal	Instruments and Experimental Techniques
Volume	53
Issue number	1
DOIs	https://doi.org/10.1134/S0020441210010288
Publication status	Published - 01 Jan 2010

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All Science Journal Classification (ASJC) codes

Instrumentation

Cite this

Mohammed, H. A., Salleh, H., & Yusoff, M. Z. (2010). Fast response surface temperature sensor for hypersonic vehicles ¹. Instruments and Experimental Techniques, 53(1), 153-159. https://doi.org/10.1134/S0020441210010288

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10.1134/S0020441210010288