This paper provides heat transfer enhancement and flow friction data for swirl flows enter tangentially to an annulus roughened with helical-ribs. The effects of the roughness intensity, tangential to total momentum flux ratio and Reynolds number were studied. The tested annulus has a radius ratio of 0.25 with the inner surface insulated and the outer one was heated with a uniform heat flux. The inner surface of the outer tube was roughened with helically coiled wires which act as turbulence promoters breaking up the viscous sublayer formed in the fluid region nearest to the wall. Roughness was made by using helical-wires at two different diameter to pitch ratios (d/p) of 0.025 and 0.050 within a range of Reynolds number from 5x103 to 25x103, and at values of the tangential to total momentum flux ratios of 1.73, 2.94, 3.46 and 5.88. It was found that there is a significant enhancement in the heat transfer due to inlet injection swirl compared with that gained by helical roughness. Also, the efficiency index is critically dependent on the roughness Reynolds number, momentum flux ratio and the roughness intensity and it is almost less than that for the rough plain annulus. New correlations for Nusselt number enhancement ratio and the Fanning friction factor ratio were obtained as functions of Reynolds number, momentum flux and d/p ratios. Also, a maximum Nusselt number enhancement ratio of about 2.0 was found corresponding to 8.7 fold increase in the flow friction factor for a single entry injector with Mt/MT of 5.88 at relatively dense roughness with d/p of 0.05.
ABDEL-MONEIM, S., EL-SHAMY, A., & BERBISH, N. (2001). HEAT TRANSFER TO A TANGENTIALLY INJECTED SWIRL FLOW THROUGH AN ARTIFICIALLY ROUGHENED ANNULUS. International Conference on Aerospace Sciences and Aviation Technology, 9(ASAT Conference, 8-10 May 2001), 1-18. doi: 10.21608/asat.2001.24852
MLA
S. A. ABDEL-MONEIM; A. R. EL-SHAMY; N. S. BERBISH. "HEAT TRANSFER TO A TANGENTIALLY INJECTED SWIRL FLOW THROUGH AN ARTIFICIALLY ROUGHENED ANNULUS". International Conference on Aerospace Sciences and Aviation Technology, 9, ASAT Conference, 8-10 May 2001, 2001, 1-18. doi: 10.21608/asat.2001.24852
HARVARD
ABDEL-MONEIM, S., EL-SHAMY, A., BERBISH, N. (2001). 'HEAT TRANSFER TO A TANGENTIALLY INJECTED SWIRL FLOW THROUGH AN ARTIFICIALLY ROUGHENED ANNULUS', International Conference on Aerospace Sciences and Aviation Technology, 9(ASAT Conference, 8-10 May 2001), pp. 1-18. doi: 10.21608/asat.2001.24852
VANCOUVER
ABDEL-MONEIM, S., EL-SHAMY, A., BERBISH, N. HEAT TRANSFER TO A TANGENTIALLY INJECTED SWIRL FLOW THROUGH AN ARTIFICIALLY ROUGHENED ANNULUS. International Conference on Aerospace Sciences and Aviation Technology, 2001; 9(ASAT Conference, 8-10 May 2001): 1-18. doi: 10.21608/asat.2001.24852
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