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The calibration of a surface static tube

Published online by Cambridge University Press:  04 July 2016

J. L. Sproston  and
Ö. T. Göksel
J. L. Sproston
Affiliation:
Fluid Mechanics Division, Department of Mechanical Engineering, University of Liverpool
Ö. T. Göksel
Affiliation:
Fluid Mechanics Division, Department of Mechanical Engineering, University of Liverpool
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Extract

The usual method of determining the static pressure distribution about a model under test often relies on guessing the required positions of the static holes before the form of the distribution is known, and subsequently adding further holes to the model where particular interest may arise. This technique can clearly prove both tedious and expensive.

Therefore interest lies in the accuracy of representation of static pressure obtained from a static tube lying on the model surface.

Type
Technical notes
Information
The Aeronautical Journal , Volume 76 , Issue 734 , February 1972 , pp. 101 - 103
Copyright
Copyright © Royal Aeronautical Society 1972 

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Footnotes

*

Now at METU Mechanical Engineering Department, Ankara Turkey.

References

1. Sproston, J. L. The Hodograph method of solution for the incompressible flow past aerofoils. Ph.D. Thesis, University of Liverpool, 1968.Google Scholar
2. Göksel, Ö. T. Some effects of spherical roughness upon the incompressible flow of a boundary layer with a zero pressure gradient. Ph.D. Thesis, University of Liverpool, 1968.Google Scholar