Surface heat-transfer coefficients of finned cylinders (1939)
NASA Technical Reports Server (NTRS) · leaf 1
description of the cylinders tested and the air-flow arrangements used is given in table I. TABLE I.—Cylinders tested Fiqu&b l.—Section showing significance of id, t, n, and (. of 0.67 inch, and an average fin thickness of 0.035 inch. The designations corresponding to the cylinders in table I can… … (a) Baffle. (b) Jacket. Figure 2.—Type of baffle and Jacket used in tunnel and blower-cooling tests. The ratio of the area of the exit to the area between the fins was approximately 2. The apparatus used in the blower-cooling tests is 1 Numbers Indicate: 1, cylinder in free air stream, no baffles.…
NASA Technical Reports Server (NTRS)
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