Energy Loss, Velocity Distribution, and Temperature Distribution for a Baffled Cylinder Model, Special Report (1937)
NASA Technical Reports Server (NTRS) · leaf 26
0 2 4 6 8 10 12 14 Exit-duct length, inches figure 13.- Effect of exit-duct length on loss in total head at 150° from front of cylinder for several baffle openings at optimum exit-duct opening. Cylinder diameter, 7.00 inches; fin space, l/4 inch.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
