Effect of heating and inlet geometry on the fully developed pressure drop in the transition region of a horizontal tube

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	Effect of heating and inlet geometry on the fully developed pressure drop in the transition region of a horizontal tube
	Tam L.-M.; Ghajar A.J.
	1996-12-01
Source Publication	American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD
ISSN	02725673
Volume	324 Pages:165-174
Abstract	Pressure drop measurements were made with a differential pressure transducer in the fully developed region of a horizontal circular straight tube with reentrant, square-edged, and bell-mouth inlets under isothermal and non-isothermal (uniform wall heat flux) flow conditions. The inlet Reynolds number for the ethylene glycol-water mixtures throughout the experiments ranged from about 1000 to 17000 to cover laminar, transition, and turbulent regimes. The isothermal fully developed skin friction coefficients showed that the range of Reynolds number values for which transition flow exists is about 2900-3500 for the reentrant inlet, 3100-3700 for the square-edged inlet, and 5100-6100 for the bell-mouth inlet. Different heat fluxes (3, 8, and 16 kW/m) were applied to the test section in order to investigate the effect of heating on the skin friction coefficient. The results indicated that the value of fully developed skin friction coefficient increased with an increase in the heating rate for a fixed Reynolds number. Due to the presence of secondary flow, the effect of heating on the skin friction coefficient is significant in the laminar and transition regions. This increase in skin friction coefficient causes an increase in the lower and upper limits of the isothermal transition boundaries. For example, for the 16 kW/m heat flux, the transition boundaries increased to about 4100-5900 for the reentrant inlet, 4500-6400 for the square-edged inlet, and 7300-9600 for the bell-mouth inlet. Available correlations for prediction of non-isothermal fully developed skin friction coefficients are compared with our experimental data. Correlations for prediction of the non-isothermal fully developed skin friction coefficients in the laminar and transition regions for the three inlets are recommended. The effect of heating in these correlations was accounted for in terms of a bulk to wall viscosity ratio expressed as a function of Prandtl and Grashof numbers.
URL	View the original
Language	英語English
Fulltext Access	View Full-Text via Scopus
Document Type	Journal article
Collection	University of Macau
Affiliation	Oklahoma State University - Stillwater
Recommended Citation GB/T 7714	Tam L.-M.,Ghajar A.J.. Effect of heating and inlet geometry on the fully developed pressure drop in the transition region of a horizontal tube[J]. American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD, 1996, 324, 165-174.
APA	Tam L.-M.., & Ghajar A.J. (1996). Effect of heating and inlet geometry on the fully developed pressure drop in the transition region of a horizontal tube. American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD, 324, 165-174.
MLA	Tam L.-M.,et al."Effect of heating and inlet geometry on the fully developed pressure drop in the transition region of a horizontal tube".American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD 324(1996):165-174.

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