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Wall Interference Effects of Static Pressure Probes in an Incompressible Turbulent Boundary Layer

Published online by Cambridge University Press:  07 June 2016

J-D Vagt  and
H H Fernholz
J-D Vagt
Affiliation:
Technische Universität, Berlin
H H Fernholz
Affiliation:
Technische Universität, Berlin
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Summary

Measurements of static pressure across the boundary layer on the wall of a circular cylinder with flow parallel to its axis display wall-interference effects which exceed corrections due to turbulence by almost an order of magnitude. Two different types of static pressure probe were investigated and gave different pressure distributions in the same boundary layer.

Type
Research Article
Information
Aeronautical Quarterly , Volume 28 , Issue 3 , August 1977 , pp. 176 - 184
Copyright
Copyright © Royal Aeronautical Society. 1977

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References

1 Barat, M Pressure measurements in highly turbulent flows. Paper given at the International Summer School for Heat and Mass Transfer, Herceg Novi, Jugoslavia, September 1969.Google Scholar
2 Toomre, A The effect of turbulence on static pressure measurements. ARC 22 010, 1960.Google Scholar
3 Bradshaw, P Goodman, D G The effect of turbulence on static pressure tubes. ARC R & M 3527, 1968.Google Scholar
4 East, L F Measurements of the three-dimensional incompressible turbulent boundary layer included on the surface of a slender delta wing by the leading edge vortex. Royal Aircraft Establishment Technical Report 73 141, 1974.Google Scholar
5 Fernholz, H Vagt, J-D Experimental investigation of three-dimensional incompressible turbulent boundary layers. Paper 2.2.3, Anglo-German Meeting on Non-Hypersonic Boundary Layers, London, September 1971.Google Scholar
6 Salter, C Worshap, J H Goodman, D G A discussion of pitot-static tubes and of their calibration factors with a description of various versions of a new design. ARC R & M 3365, May 1962.Google Scholar
7 van den Berg, B Elsenaar, A Measurements in a three-dimensional incompressible turbulent boundary layer in an adverse pressure gradient under infinite swept wing conditions. NLR (Amsterdam) TR 72092 U, 1972.Google Scholar
8 Froebel, E Power supply and computer unit for the Statham pressure transducer. Internal report, DFVLR-Berlin, 1972.Google Scholar
9 Froebel, E Vagt, J-D Ein automatisch abgleichendes Flüssigkeitsmanometer mit digitaler Anzeige. DLR-FB 74-40, 1974.Google Scholar
10 Rotta, J C Turbulente Strömungen, p 178. B G Teubner Verlag, 1972.CrossRefGoogle Scholar
11 Goldstein, S A note on the measurement of total head and static pressure in a turbulent stream. Proc. Roy. Soc. A, Vol 155, p 570, 1936.Google Scholar
12 Fage, A On the static pressure in fully-developed turbulent flow. Proc. Roy. Soc. A, Vol 155, p 576, 1936.Google Scholar
13 Rechenberg, I Zur Messung der turbulenten Wandreibung mit dem Prestonrohr. Jahrbuch der WGLR, 1962.Google Scholar
14 Klebanoff, P S Characteristics of turbulence in a boundary layer with zero pressure gradient. NACA Report 1247, 1955.Google Scholar
15 Fiedler, H Theoretische und experimentelle Analyse des statischen Druckes im ebenen turbulenten Freistrahl bei kleiner Mach-Zahl. DLR-FB 67/04, 1967.Google Scholar
16 Fernholz, H Geschwindigkeitsprofile, Temperaturprofile und halbempirische Gesetze in kompressiblen turbulenten Grenzschichten bei konstantem Druck. Ingenieur Archiv, Vol 38, p 311, 1969.Google Scholar