Abstract
An improved version of Campbell and Slattery's solution for the developing laminar pipe flow is presented. The analysis provides slightly better over-all flow description.
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Abbreviations
- p :
-
pressure
- p 0 :
-
pressure at the entry cross section
- p*:
-
dimensionless pressure, (p 0−p)/ρV 2
- r, x :
-
cylindrical coordinates
- Q :
-
volume rate of flow through tube
- R :
-
tube radius
- u, v :
-
velocity components in the axial and radial directions respectively
- U :
-
core velocity
- V :
-
average velocity, Q/πR 2
- X*:
-
dimensionless axial distance x/(R 2 Vρ/μ)
- δ :
-
boundary layer thickness
- μ :
-
viscosity
- ρ :
-
density
References
Campbell, W. D. and J. C. Slattery, Trans. ASME J. Basic Eng. 85 D (1963) 41.
Volkov, V. N., J. of Eng. Physics, Vol. 9 (1965) 371.
Campbell, W. D., MS thesis, Northwestern Univ., 1960.
Prandtl, L. and O. G. Tietjens, Applied Hydro- and Aeromechanics, McGraw Hill Book Company, Inc., N. Y., 1934, p. 27.
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Gupta, R.C. Laminar flow in the entrance of a tube. Appl. Sci. Res. 33, 1–10 (1977). https://doi.org/10.1007/BF00383189
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DOI: https://doi.org/10.1007/BF00383189