Tests of Spheres with Reference to Reynolds Number, Turbulence, and Surface Roughness (1935)
NASA Technical Reports Server (NTRS) · leaf 33
N.A.C.A. Technical Memorandum No. 777 Figs. 1,2,3,4,5 Pot entity/ theory a, Disk —Sub-criticol R=-p2iQS cw = 1.20 ^-Super critical ft. Sphere sub critical cw - 0.47 Sphere euper critical Figure 2.- Pressure distribution cw = 0.08 over sphere (ref. 3). d, Spindle shape cw = 0.04 Figure 1.- Flow… … t* * J * 8 Figure 3.- Effect of support method in the wake of the sphere on its drag. Figure 5. Effect of rear spindle on sphere drag.
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