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Principles involved in the cooling of a finned and baffled cylinder (1938)

NASA Technical Reports Server (NTRS) · leaf 22

An illustration from Principles involved in the cooling of a finned and baffled cylinder, 1938, leaf 22 — Vigors 10.- Variation of optimum fin thickness with spacing for four fin widths. Steel cylinder; 1^= 2.17 B.t.u./hr.sq.in.°F

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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