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Principles involved in the cooling of a finned and baffled cylinder (1938)
NASA Technical Reports Server (NTRS) · leaf 17
.0011 1—I—l—LJ « 1—I—1,1 I U—I—LJ_I 1—I—L_LJ 1 !—I—Mill—I—I 10 20 30 40 60 80 100 800 30u 400 600 800 h- Velocity, 7, f.p.s. tfigure 5.- Variation of heat-transfer coefficient with velocity at constant diameter. 01NASA Technical Reports Server (NTRS)
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