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Heat-transfer coefficients for air flowing in round tubes, in rectangular ducts, and around finned cylindersReport reviews published data and presents some new data on heat transfer to air flowing in round tubes, in rectangular ducts, and around finned cylinders. The available data for heat transfer to air in straight ducts of rectangular and circular cross section have been correlated in plots of Stanton number versus Reynolds number to provide a background for the study of the data for finned cylinders. Equations are recommended for both the streamlined and turbulent regions, and data are presented for the transition region between turbulent and laminar flow. Use of hexagonal ends on round tubes causes the characteristics of laminar flow to extend to high Reynolds numbers. Average coefficients for the entire finned cylinder have been calculated from the average temperature at the base of the fins and an equation which was derived to allow for the effectiveness of the fins. The available results for each finned cylinder are correlated herein in terms of graphs of Stanton number versus Reynolds number. In general, for a given Reynolds number, the Stanton number increases with increases in both spacing and width of the fins, and is apparently independent of cylinder diameter and temperature difference. For a given coefficient of heat transfer improved baffles and rough or wavy surfaces give a substantial reduction in pumping power per unit of heat transfer surface and a somewhat smaller decrease in pressure drop. (author)
Document ID
19930090924
Document Type
Other
Authors
Drexel, Rober E
Mcadams, William H
Date Acquired
September 6, 2013
Publication Date
February 1, 1945
Report/Patent Number
NACA-WR-W-108
NACA-ARR-4F28
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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NameType 19930090924.pdf STI