Heat transfer and skin friction for turbulent boundary-layer flow longitudinal to a circular cylinder

E. M. Sparrow, R. G.E. Eckert, W. J. Minkowycz

Research output: Contribution to journalArticle

5 Citations (Scopus)

Abstract

An analysis has been carried out for the turbulent velocity and thermal boundary layers which develop along a cylinder whose axis is parallel to the free-stream flow. Local and average friction factors are calculated as functions of the length Reynolds number Rex for various cylinder sizes (characterized, by the radius Reynolds number Rer0). For corresponding flow conditions, the friction factor for a cylinder always exceeds that for the flat plate. Local heat-transfer coefficients corresponding to the case of uniform wall heat flux have been obtained for Prandtl numbers of 0.7 and 5. As with the friction factors, the cylinder heat-transfer coefficients exceed those for the flat plate. This effect of the cylindrical geometry on heat transfer diminishes with increasing Prandtl number.

Original languageEnglish (US)
Pages (from-to)37-43
Number of pages7
JournalJournal of Applied Mechanics, Transactions ASME
Volume30
Issue number1
DOIs
StatePublished - Jan 1 1960

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skin friction
boundary layer flow
Skin friction
Boundary layer flow
turbulent boundary layer
circular cylinders
Circular cylinders
friction factor
friction
heat transfer
Prandtl number
Friction
Heat transfer
Heat transfer coefficients
Reynolds number
flat plates
heat transfer coefficients
Stream flow
thermal boundary layer
Heat flux

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Heat transfer and skin friction for turbulent boundary-layer flow longitudinal to a circular cylinder. / Sparrow, E. M.; Eckert, R. G.E.; Minkowycz, W. J.

In: Journal of Applied Mechanics, Transactions ASME, Vol. 30, No. 1, 01.01.1960, p. 37-43.

Research output: Contribution to journalArticle

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