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contributor authorH. C. Reynolds
contributor authorT. B. Swearingen
contributor authorD. M. McEligot
date accessioned2017-05-09T00:22:43Z
date available2017-05-09T00:22:43Z
date copyrightMarch, 1969
date issued1969
identifier issn0098-2202
identifier otherJFEGA4-27327#87_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135223
description abstractThe thermal entrance problem for low Reynolds number, turbulent flow of gases in circular tubes is solved analytically by the method of Sparrow, Hallman, and Siegel. Fluid properties are considered constant. The solution is based on a Reynolds-number-dependent velocity profile developed, in a companion paper, by modifying Reichardt’s wall and middle law eddy diffusivity expressions. Tabular values of the eigenvalues and normalized Nusselt numbers are presented for a range of Reynolds numbers from 3,000 to 50,000. The axial variation of Nusselt number is found to be correlated by NuNu∞ = 1 + 0.8(1+70,000 Re−3/2) xD−1 to within ±5 percent for x/D ≥ 2. The fully developed value agrees with the Dittus-Boelter correlation. For the eigenvalues, λn 2 , and the associated constants, An , correlations of the form λn2 = a1,n Re−b1,n + c1,n Re−d1,nAn = a2,n Re−b2,n + c2,nRe−d2,n are obtained. Heat transfer data are presented, primarily for helium, for the conditions of the analysis. In the low Reynolds number turbulent regime, these data clearly support the present analytical solution.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermal Entry for Low Reynolds Number Turbulent Flow
typeJournal Paper
journal volume91
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3571033
journal fristpage87
journal lastpage94
identifier eissn1528-901X
keywordsTurbulence
keywordsReynolds number
keywordsEigenvalues
keywordsHelium
keywordsEddies (Fluid dynamics)
keywordsHeat transfer
keywordsFluids AND Gases
treeJournal of Fluids Engineering:;1969:;volume( 091 ):;issue: 001
contenttypeFulltext


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