Method for calculation of heat transfer in laminar region of air flow around cylinders of arbitrary cross section (including large temperature differences and transpiration cooling)

E. R. G. Eckert, John N. B. Livingood
naca-tn-2733
Jun 1952


The solution of heat-transfer problems has become vital for many aeronautical applications. The shapes of objects to be cooled can often be approximated by cylinders of various cross sections with flow normal to the axis as, for instance, heat transfer on gas-turbine blades and on airfoils heated for deicing purposes.

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