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U.S. Department of Energy
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RESEARCH ON HEAT TRANSFER TO FLUIDS FLOWING THROUGH NON-CIRCULAR CHANNELS. Progress Report, September 1960-March 1961

Technical Report ·
OSTI ID:4060438
Turbulent heat transfer was measured in rectangular ducts of aspect ratio 1: 1 having a thermal boundary condition of two vertical walls approximating an adiabatic boundary and two horizontal walls approximating a constant heat flux boundary. Measurements were made to determine the low Reynolds number limit, the bulk temperature rise consistent with constant property assumption and structural limitations, and the heat transfer coefficient as a function of distance along the axis of the duct. The centerline temperature distribution of the heated walls for a heat transfer run with a bulk temperature rise of 61.8 deg F. The Nusselt number was calculated from the fully developed heat transfer coefficient, the hydraulic diameter, and the thermal conductivity based on the average bulk temperature for the duct. Heat transfer for flow in rectangular ducts was also calculated for the following boundary conditions: constant wall temperature peripherally with constant axial heat flux and constant axial and peripheral heat flux. The calculations were carried out by use of the Deissler method. (M.C.G.)
Research Organization:
Minnesota. Univ., Minneapolis. Heat Transfer Lab.
NSA Number:
NSA-15-014392
OSTI ID:
4060438
Report Number(s):
TID-12310
Country of Publication:
United States
Language:
English