Hostname: page-component-78c5997874-8bhkd Total loading time: 0 Render date: 2024-11-04T19:51:47.075Z Has data issue: false hasContentIssue false

Characteristics of turbulent boundary layers at low Reynolds numbers with and without transpiration

Published online by Cambridge University Press:  29 March 2006

Roger L. Simpson
Affiliation:
Institute of Technology, Southern Methodist University, Dallas, Texas

Abstract

An extension to Coles's (1956) ‘law of the wall–law of the wake’ formulation for incompressible unblown boundary layers with momentum thickness Reynolds number Reθ > 6000. is made for Reθ < 6000. It is found that κ = 0·40, the von Kármán constant for Reθ > 6000, is replaced by Ω = 0·40 (Reθ/6000) for Reθ < 6000. Based upon the data of Simpson (1967) this formulation is extended to injection and undersucked (dθ/dx > 0) flows in ‘law of the wall’ and ‘velocity-defect’ representations. This law of the wall for the logarithmic turbulent region and Reichardt's sublayer variation of εM/ν are used to obtain a continuous expression for εM/ν as a function of U+, V+w, and Reθ for the wall region. This expression is in reasonable agreement with the generated εM/ν blowing results and in less agreement with the unblown and suction results. Eddy viscosity and mixing length results confirm that εM/δ*U ∝ Ω2 and l/δ ∝ Ω for the outer region and that εM/δ*U and l/δ are substantially independent of blowing and moderate suction, as also reflected by the velocity defect representation for injection and suction.

Type
Research Article
Copyright
© 1970 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

Black, T. J. & Sarnecki, A. J. 1958 Aero. Res. Counc. Rep. 20, 501, F.M. 2745; also 1965 Aero. Res. Counc. R & M 3387.
Bradshaw, P. 1967 J. Fluid Mech. 29, 62.
Bradshaw, P., Ferriss, D. H. & Atwell, D. A. 1967 J. Fluid Mech. 28, 59.
Clark, J. H., Henkes, H. R. & Libby, P. A. 1955 J. Aero. Sci. 22, 25.
Coles, D. 1956 J. Fluid Mech. 1, 19.
Coles, D. 1962 Rand Rep. R-403-PR.
Dahm, T. J. & Kendall, R. M. 1968 AIAA J. 6, 182.
Dershin, H., Leonard, C. A. & Gallaher, W. A. 1967 AIAA J. 5, 1934.
Dorrance, W. J. & Dore, F. J. 1954 J. Aero. Sci. 21, 10.
Escudier, M. P. 1965 Imperial College. Mech. Engrg. Rep., TWF/TN/1.
Favre, A., Dumas, R., Verollet, E. & Coantic, M. 1966 J. de Mécanique 5, 3.
Fraser, M. D. 1964 Sc.D. Thesis, MIT.
Hinze, J. O. 1959 Turbulence. New York: McGraw-Hill.
Kendall, R. M. 1959 Sc.D. Thesis, MIT.
Kendall, R. M., Rubesin, M. W., Dahm, T. J. & Mendenhall, M. R. 1964 Vidya, Palo Alto, Calif., Vidya Rep. 111 (AD 69 209).
Kinney, R. B. 1967 AIAA J. 5, 62.
Klebanoff, P. S. 1954 NACA TN 3178.
Kleinstein, G. 1967 AIAAA J. 5, 140.
Kline, S. J. 1965 Proc. Inst. Mech. Engrs. 180, 22.
Kline, S. J., Cockrell, D. J. & Morkovin, M. V.(ed.) 1968 Proc. 1968 Conf. on Turbulent Boundary Layer Prediction. 1.
Mcquaid, J. 1966 Ph.D. Thesis, Cambridge University.
Mickley, H. S. & Davis, R. S. 1957 NACA TN 4017.
Mickley, H. S., Ross, R. C., Squyers, A. L. & Stewart, W. E. 1954 NACA TN 3208.
Mickley, H. S. & Smith, K. A. 1963 AIAA J. 1, 168.
Mickley, H. S., Smith, K. A. & Fraser, M. D. 1964 AIAA J. 2, 17.
Mickley, H. S., Smith, K. A. & Fraser, M. D. 1965 AIAA J. 3, 78.
Moffat, R. J. & Kays, W. M. 1967 Stanford University, Mech. Engrg. Rep. HMT-1; also 1968 Int. J. Heat Mass Trans. 11, 154.
Rotta, J. C. 1962 Progress in Aero. Sciences, 2, 1. New York: MacMillan.
Rotta, J. C. 1966 Deutsche Luft und Raumfahrt Forsch. ber. 6, 4.
Rubesin, M. W. 1954 NACA TN 3341.
Schubauer, G. G. 1954 J. Appl. Phys. 25, 18.
Simpson, R. L. 1967 Ph.D. Thesis, Stanford University; available from University Microfilms, Ann Arbor, Mich.
Simpson, R. L., Moffat, R. J. & Kays, W. M. 1969 Int. J. Heat Mass Trans. 12, 77.
Simpson, R. L. & Whitten, D. G. 1968 AIAA J. 6, 177.
Simpson, R. L., Whitten, D. G. & Moffat, R. J. 1970 Int. J. Heat Mass Trans. 13, 12.
Smith, K. A. 1962 Sc.D. Thesis, MIT.
Spalding, D. B. 1961 TASME J. Appl. Mech. 28, 45.
Stevenson, T. N. 1963a Cranfield Coll. of Aero., Aero. Rep. 166.
Stevenson, T. N. 1963b Cranfield Coll. of Aero., Aero. Rep. 170.
Stevenson, T. N. 1964 Cranfield Coll. of Aero., Aero. Rep. 177.
Stevenson, T. N. 1968 AIAA J. 6, 55.
Torii, K., Nishiwaki, N. & Hirata, M. 1966 Proc. Third Inter. Heat Transfer Conf. 3, 3.
Whitten, D. G. 1967 Ph.D. Thesis, Stanford University; available from University Microfilms. Ann Arbor, Mich.
Whitten, D. G., Kays, W. M. & Moffat, R. J. 1970 Int. J. Heat Mass Trans. (To be published.)
Wieghardt, K. 1943 Göettingen U & M Rept. 6603.
Wooldridge, C. E. & Muzzy, R. J. 1966 AIAA J. 11, 200.