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Blower Cooling of Finned Cylinders (1937)

NASA Technical Reports Server (NTRS) · leaf 12

An illustration from Blower Cooling of Finned Cylinders, 1937, leaf 12
9 BLOWER COOLING OF FINNED CYLINDERS same weight velocity of the air except for the 0.166 as are shown in figure 11, where is the total power cyUnder. The data for the 0.166 cyUnder fell on the loss across the jacket and includes both Ft and the same curve as the data for the 0.137-inch pitch… … Vnxp^q ,lb./sec./sq.ff. -EfTect of weight velocity of the cooling air on Pt{p\qy-\w. FlGlRE 11. power would be I'equired to force air by more widely .00001 2 3 4 5 6 7 8 3/0 i spaced fins. An analysis of the pressure drops around VmP.g Jb./sec./sq.ft. cylinders to be presented in a later report…

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