The Effect of Baffles on the Temperature Distribution and Heat-transfer Coefficients of Finned Cylinders (1936)
NASA Technical Reports Server (NTRS) · leaf 15
d from 298° F. for a cylinder with possible, when the entrance was equal to the arc sub- straight fins and no baffles to 210° F., or 29.G percent, tended by an angle of approximately 145°, when the as compared with the 31.9 percent reduction obtained rearward extensions were 3 or more inches long,… … 42 BC+A at 30° .1057 . 554 149.4 112.1 C. Bent fins, no baffles 200.9 Figure 21.—Cylinder-wall temperatures and heat D. Bent fins, with baffles _ 170.0 Figure 19—Effect of strips between shell baffles and transfer coefficients obtained with integral baffles fin tips on the temperature distribution…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.