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Two Probes for the Measurement of the Complete Velocity Vector in Subsonic Flow

Published online by Cambridge University Press:  04 July 2016

K. Dau ,
M. McLeod  and
D. Surry
K. Dau
Affiliation:
Institute for Aerospace Studies, University of Toronto
M. McLeod
Affiliation:
Institute for Aerospace Studies, University of Toronto
D. Surry
Affiliation:
Institute for Aerospace Studies, University of Toronto
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Extract

Two probes which have been developed at the University of Toronto's Institute for Aerospace Studies for the purpose of determining the complete velocity vector in subsonic flow are described. That is, both probes provide the magnitude of the velocity at a point plus the two angles which determine the vector's orientation. The first probe, which also measures static pressure, was developed by K. Dau to determine wake properties behind a blowing wing. It uses a multiple pressure-hole technique. The second probe was originated by K. Dau and D. Surry and experimentally developed by M. McLeod. It is basically a spinning hot-wire probe whose periodic waveform uniquely defines the complete velocity vector.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 72 , Issue 696 , December 1968 , pp. 1066 - 1068
Copyright
Copyright © Royal Aeronautical Society 1968 

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References

1. UTIAS Annual Progress Report, Oct 1965, Section F-L p45.Google Scholar
2. UTIAS Annual Progress Report, Oct 1965, Section F-7, p47.Google Scholar
3. UTIAS Annual Progress Report, Oct 1966, Section F-7, p 54.Google Scholar
4. UTIAS Annual Progress Report, Oct 1967, Section F-5, p52.Google Scholar
5. Chu, W. T. UTIAS Report No 119: Turbulence Measurements Relevant to Jet Noise. Nov 1966.Google Scholar
6. McLeod, M. UTIAS TN 125: A Spinning Hot-Wire Anemometer for Simultaneous Measurement of u, v and w. January, 1968.Google Scholar