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Measurements in the thick axisymmetric turbulent boundary layer near the tail of a body of revolution

Published online by Cambridge University Press:  29 March 2006

V. C. Patel ,
A. Nakayama  and
R. Damian
V. C. Patel
Affiliation:
Institute of Hydraulic Research, University of Iowa, Iowa City, Iowa 52242
A. Nakayama
Affiliation:
Institute of Hydraulic Research, University of Iowa, Iowa City, Iowa 52242
R. Damian
Affiliation:
Institute of Hydraulic Research, University of Iowa, Iowa City, Iowa 52242
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Abstract

Detailed measurements of pressure distributions, mean velocity profiles and Reynolds stresses were made in the thick axisymmetric turbulent boundary layer near the tail of a body of revolution. The results indicate a number of important differences between the behaviour of a thick and a thin boundary layer. The thick boundary layer is characterized by significant variations in static pressure across it and an abnormally low level of turbulence. The static-pressure variation is associated with a strong interaction between the boundary layer and the potential flow outside it, while the changes in the turbulence structure appear to be a consequence of the transverse surface curvature. In order to predict the behaviour of the flow in the tail region of a body of revolution it is not therefore possible to use conventional thin-boundary-layer calculation procedures.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 63 , Issue 2 , 3 April 1974 , pp. 345 - 367
Copyright
© 1974 Cambridge University Press

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References

Bradsraw, P., Ferriss, D. H. & Atwell, N. P. 1967 Calculation of boundary layer development using the turbulent energy equation. J. Fluid Mech. 28, 593.Google Scholar
Cebeci, T. 1970 Laminar and turbulent incompressible boundary layers on slender bodies of revolution in axial flow. J. Basic Engng, Trans. A.S.M.E. D 92, 545.Google Scholar
Chevray, R. 1968 The turbulent wake of a body of revolution. J. Basic Engng, Trans. A.S.M.E. D 90, 275.Google Scholar
Clauser, F. H. 1956 The turbulent boundary layer. Adv. in Appl. Mech. 4, 1.Google Scholar
Glover, J. R. 1972 'Old Gold Model, Type 4-2H Hot-wire Anemometer' and ‘Type 2 Mean-Product Computer’. Iowa Inst. Hydraul. Res. Rep. no. 136.
Klebanoff, P. S. 1955 Characteristics of turbulence in a boundary layer with zero pressure gradient. N.A.C.A. Tech. Rep. no. 1247.
Laufer, J. 1954 The structure of turbulence in fully developed pipe flow. N.A.C.A. Tech. Rep. no. 1174.
Naudascher, E. 1964 Effect of density on air-tunnel measurements. J. Roy. Aero. Soc. 68, 419.Google Scholar
Patel, V. C. 1965 Calibration of the Preston tube and limitations on its use in pressure gradients. J. Fluid Mech. 23, 185.Google Scholar
Patel, V. C. 1973a A unified view of the law of the wall using mixing-length theory. Aero. Quart. 24, 55.Google Scholar
Patel, V. C. 1973b On the equations of a thick axisymmetric turbulent boundary layer. Iowa Inst. Hydraul. Res. Rep. no. 143.
Richnond, R. L. 1957 Experimental investigation of thick axially symmetric boundary layers on cylinders at subsonic and hypersonic speeds. Ph.D. Thesis, California Institute of Technology, Pasadena.
Satija, K. S. 1971 On the thick boundary layer near the tail of a body of revolution. Ph.D. Thesis, University of Iowa, Iowa City.
Thompson, B. G. J. 1965 A new two-parameter family of mean velocity profiles for incompressible turbulent boundary layers on smooth walls. Aero. Res. Counc. R. & M. no. 3463.
Yasuhara, M. 1959 Experiments of axisymmetric boundary layers along a cylinder in incompressible flow. Trans. Japan Soc. Aerospace Sci. 2, 33.Google Scholar