The steady, buoyancy-driven, laminar motion induced in the annulus of two horizontal, concentric, circular cylinders by a difference in the boundary temperatures is studied analytically in the large Rayleigh number limit. The flowfield is divided into five physically distinct regions: (1) an inner free convection boundary layer near the inner cylinder, (2) an outer free convection boundary layer near the outer cylinder, (3) a vertical plume above the inner cylinder, (4) a stagnant region below the inner cylinder, and (5) a core region surrounded by the other four regions. Zeroth-order solutions which account for the coupling of those five regions are obtained in the high Prandtl number limit using a boundary-layer approximation and integral methods. Comparisons of the calculated heat transfer and temperature fields with experiment and numerical finite-difference results are favorable.
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Boundary Layer Regime for Laminar Free Convection between Horizontal Circular Cylinders
M. C. Jischke,
M. C. Jischke
School of Aerospace, Mechanical, and Nuclear Engineering, University of Oklahoma, Norman, Okla.
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M. Farshchi
M. Farshchi
School of Aerospace, Mechanical, and Nuclear Engineering, University of Oklahoma, Norman, Okla.
Search for other works by this author on:
M. C. Jischke
School of Aerospace, Mechanical, and Nuclear Engineering, University of Oklahoma, Norman, Okla.
M. Farshchi
School of Aerospace, Mechanical, and Nuclear Engineering, University of Oklahoma, Norman, Okla.
J. Heat Transfer. May 1980, 102(2): 228-235 (8 pages)
Published Online: May 1, 1980
Article history
Received:
September 21, 1979
Online:
October 20, 2009
Citation
Jischke, M. C., and Farshchi, M. (May 1, 1980). "Boundary Layer Regime for Laminar Free Convection between Horizontal Circular Cylinders." ASME. J. Heat Transfer. May 1980; 102(2): 228–235. https://doi.org/10.1115/1.3244265
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