Hostname: page-component-848d4c4894-ndmmz Total loading time: 0 Render date: 2024-05-18T04:29:35.871Z Has data issue: false hasContentIssue false

The measurement of skin friction in turbulent boundary layers with adverse pressure gradients

Published online by Cambridge University Press:  28 March 2006

K. C. Brown
Affiliation:
Department of Mechanical Engineering, University of Melbourne
P. N. Joubert
Affiliation:
Department of Mechanical Engineering, University of Melbourne

Abstract

This paper describes a floating-element skin friction meter which has been designed for use in adverse pressure gradients. The effects of secondary forces on the element, which arise from the pressure gradient, are examined in some detail. The limitations of various methods of measuring wall shear stress are discussed and the results from the floating element device are compared with measurements taken in a two-dimensional boundary layer using Preston tubes and velocity profiles. As it is planned to use the instrument later for direct measurements of the shear stress in three-dimensional boundary layers, the relevance of the instrument to this situation is also discussed.

Type
Research Article
Copyright
© 1969 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Bellhouse, B. J. & Schultz, D. L. 1964 Aero. Res. Counc. R & M, no. 3445.
Bidwell, J. M. 1951 NACA TN 2571.
Bradshaw, P. 1959 J. Aero Space Sci. 26, 841.
Brown, G. L. 1967 Heat Trans. Fluid Mech. Inst. Proc.
Clauser, F. H. 1954 J. Aero Sci. 21, 91.
Coles, D. 1953 Ph.D. Thesis, California Inst. of Tech.
Dhawan, S. 1953 NACA TR 1121.
Drinkuth, R. H. & Pierce, F. J. 1966 Rev. Sci. Instrum. 37, 740.
Duffy, J. & Norbury, J. F. 1967 J. Roy. Aero Soc. 71, 55.
Fage, A. & Falkner, V. M. 1930 Proc. Roy. Soc. A, 129, 378.
Ferriss, D. H. 1965 Aero. Res. Counc. CP 831.
Good, M. C. & Joubert, P. N. 1968 J. Fluid Mech. 31, 547.
Hakkinen, R. J. 1955 NACA TN 3486.
Headley, J. W. 1966 AIAA J. 4, 1862.
Head, M. R. & Rechenberg, I. 1962 J. Fluid Mech. 14, 1.
Johnston, J. P. 1957 M.I.T. Gas Turbine Lab. Rep. 39.
Joubert, P. N., Perry, A. E. & Brown, K. C. 1967 Fluid Mechanics of Internal Flow, Gino Sovran (ed.), Amsterdam: Elsevier.
Kempf, G. 1929 Werft, Reed. Hafen, 10, 234, 247.
Liepmann, H. W. & Skinner, G. T. 1954 NACA TN 3268.
Ludwieg, H. 1949 Ing. Arch. 17, 207, also NACA TM 1284.
Ludwieg, H. & Tillmann, W. 1949 Ing. Arch. 17, 288, also NACA TM 1285.
Meyer, R. F. 1966 Nat. Res. Counc. Can. Rep. LR-457.
Naleid, J. F. & Thompson, M. J. 1961 J. Aero. Space Sci. 28, 940.
Patel, V. C. 1965 J. Fluid Mech. 23, 185.
Perry, A. E. 1966 J. Fluid Mech. 26, 481.
Perry, A. E., Bell, J. B. & Joubert, P. N. 1966 J. Fluid Mech. 25, 299.
Perry, A. E. & Joubert, P. N. 1965 J. Fluid Mech. 22, 285.
Preston, J. H. 1954 J. Roy. Aero. Soc. 58, 109.
Rajaratnam, N. & Froelich, C. P. 1967 J. Roy. Aero. Soc. 71, 52.
Rechenberg, I. 1963 Z. Flugwiss. 11, 429.
Schultz-Grunow, F. 1940 Luftfahrtforschung, 17, 239.
Schlichting, H. 1962 Boundary Layer Theory, 4th ed. New York: McGraw-Hill.
Smith, P. D. 1965 Ph.D. Thesis, Univ. of Lond.
Smith, D. W. & Walker, J. H. 1959 NASA R 26.
Wyatt, L. A. & East, L. F. 1966 RAE Tech. Rep. 66027.