Surface heat-transfer coefficients of finned cylinders (1939)
NASA Technical Reports Server (NTRS) · leaf 12
to those tested in this investigation (reference linearly with that of the fluid, as is practically always 5). Faired curves of all these data are plotted in figure true for air-cooled finned cylinders, the difference be- 10. The effect of the fin width on the pressure differ- tween the average… … Space between ffns.s.ih. the results of the tests with blower cooling plotted ac- Figuej; 10.—Effect of fin space on pressure difference across finned cylinders at several cording to equation (5). Efforts to correlate the data weight velocities of the cooling air. JTn -widths from 0.37 to \£…
NASA Technical Reports Server (NTRS)
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