Heat Transfer from Finned Metal Cylinders in an Air Stream (1935)
NASA Technical Reports Server (NTRS) · leaf 11
10 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Distance from base, inches same fin space, the first having a thickness of 0.09 inch Figure 7.—Temperature difference along the fin width at the front, side, and rear and a width of 1.22 inches and the second a thickness of three cylinders tested.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
