DocumentCode :
1196730
Title :
Response or Hot Wire to Sound Pressure in an Airstream
Author :
Ko, Norman W.M. ; Ho, Kai Kwong
Volume :
23
Issue :
3
fYear :
1974
Firstpage :
211
Lastpage :
214
Abstract :
An experimental investigation of the response of hot wire to plane acoustic waves in an airstream is presented. The sensing of the pressure fluctuations by the hot wire depends on the relative magnitude between the pressure fluctuations due to the acoustic waves and the velocity fluctuations due to the local turbulence. For low turbulence the results agree well with a mathematical analysis of the problem.
Keywords :
Acoustic waves; Calibration; Difference equations; Mathematical analysis; Mechanical engineering; Steady-state; Voltage fluctuations; Wire;
fLanguage :
English
Journal_Title :
Instrumentation and Measurement, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9456
Type :
jour
DOI :
10.1109/TIM.1974.4314264
Filename :
4314264
Link To Document :
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