Effect of heating and inlet geometry on the fully developed pressure drop in the transition region of a horizontal tube
Book
·
OSTI ID:428146
- Oklahoma State Univ., Stillwater, OK (United States). School of Mechanical and Aerospace Engineering
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 isothermal fully developed skin friction coefficients showed that the range of Reynolds number values for which transition flow exists is about 2,900--3,500 for the reentrant inlet, 3,100--3,700 for the square-edged inlet, and 5100--6100 for the bell-mouth inlet. Different heat fluxes 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. Available correlations for prediction of non-isothermal fully developed skin friction coefficients are compared with the 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.
- OSTI ID:
- 428146
- Report Number(s):
- CONF-960815--; ISBN 0-7918-1506-4
- Country of Publication:
- United States
- Language:
- English
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