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 | |
| Publication status | Published - 01 Jan 2010 |
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All Science Journal Classification (ASJC) codes
- Instrumentation
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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 journal › Article
TY - JOUR
T1 - Fast response surface temperature sensor for hypersonic vehicles 1
AU - Mohammed, H. A.
AU - Salleh, H.
AU - Yusoff, M. Z.
PY - 2010/1/1
Y1 - 2010/1/1
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=77950825761&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=77950825761&partnerID=8YFLogxK
U2 - 10.1134/S0020441210010288
DO - 10.1134/S0020441210010288
M3 - Article
AN - SCOPUS:77950825761
VL - 53
SP - 153
EP - 159
JO - Instruments and Experimental Techniques
JF - Instruments and Experimental Techniques
SN - 0020-4412
IS - 1
ER -