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Remarks on transition in a round tube

Published online by Cambridge University Press:  28 March 2006

A. M. O. Smith
Affiliation:
Douglas Aircraft Company Inc., El Segundo, Califorina

Abstract

This article has a twofold purpose: (1) to analyse the available theoretical and experimental knowledge concerning flow in the inlet region of a smooth round tube, and (2) to point out that the e9 amplification factor method apparently predicts natural transition correctly over a significant fraction of the entire inlet lenght of the tube. The successful prediction indicates, but does not prove, that flow in a smooth round tube becomes turbulent at higher Reynolds numbers because transition occurs in the inlet lenght—not in the fully developed Poiseuille régime. The close agreement between theory and a test result obtained by Pfenninger indicates that the e9 method is valid for a wide variety of flows having x Reynolds numbers of transition ranging from 570,000 to 40 million. The results are applicable to both plane and axially symmetric flows.

Type
Research Article
Copyright
© 1960 Cambridge University Press

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References

Corcos, G. M. & Sellars, J. R. 1959 J. Fluid Mech. 5, 97.
Goldstein, S. (ed.) 1938 Modern Developments in Fluid Dynamics. Vol. I, Ch. VII. Oxford University Press.
Langhaar, H. L. 1942 Trans. A.S.M.E. 64, A-55.
Leite, R. J. 1959 J. Fluid Mech. 5, 81.
Lin, C. C. 1955 Theory of Hydrodynamic Stability. Cambridge University Press.
Pfenninger, W. 1950 Experiments with Laminar Flow in a Two-inch-diameter 40-foot-long Tube at high Reynolds Numbers. Northrop Aircraft Co. Rep. no. AM-128.
Pfenninger, W. 1951a Further Laminar-flow Experiments in a 40-foot-long 2-inch-Diameter Tube. Northrop Aircraft Co. Rep. no. AM-133.
Pfenninger, W. 1951b Further Laminar flow Experiments in a Tube at high Reynolds Numbers. Northrop Aircraft Co. Rep. no. AM-147.
Prandtl, L. & Tietjens, O. G. 1934 Applied Hydro- and Aeromechanics. New York: McGraw-Hill.
Punnis, B. 1947 Zur Berechnung der Laminaren Einlaufströmung im Rohr. Bericht 47P/03 Max Planck Inst. für Strömungsforschung.
Reshotko, E. 1958 Experimental Study of the Stability of Pipe Flow. 1. Establishment of an axially-symmetric Poiseuille Flow. Progress Rep. no. 20-364 Jet Propulsion Laboratory, Pasadena, California.
Schlichting, H. 1955 Boundary Layer Theory. New York: McGraw-Hill.
Smith, A. M. O. 1956a Transition, Pressure Gradient and Stability Theory. Proc. IX. Int. Congress of Appl. Mech., Brussels.
Smith, A. M. O. 1956b J. Aero. Sci. 23, 901.
Smith, A. M. O. & Gamberoni, N. 1956 Transition, Pressure Gradient and Stability Theory. Douglas Aircraft Co. Rep. no. ES 26388.
Tatsumi, T. 1952 J. Phys. Soc. Japan, 7, 489.