. Cavitation inception and internal flows with cavitation. Cavitation. (c). Figure 29 - The Effect of Freestream Turbulence on the Flow Past the NSRDC Body (The flow Is from right to left at a body Reynolds number of x 10 . The turbulence intensity is: (a) percent, (b) , (c) , (d) , and (e) percent, Gates 1977) 52. Please note that these images are extracted from scanned page images that may have been digitally enhanced for readability - coloration and appearance of these illustrations may not perfectly resemble the original Acosta, Allan J. , 1924-; David W. Tayl
. Cavitation inception and internal flows with cavitation. Cavitation. (c). Figure 29 - The Effect of Freestream Turbulence on the Flow Past the NSRDC Body (The flow Is from right to left at a body Reynolds number of x 10 . The turbulence intensity is: (a) percent, (b) , (c) , (d) , and (e) percent, Gates 1977) 52. Please note that these images are extracted from scanned page images that may have been digitally enhanced for readability - coloration and appearance of these illustrations may not perfectly resemble the original Acosta, Allan J. , 1924-; David W. Taylor Naval Ship Research and Development Center. Bethesda, Md. : David W. Taylor Naval Ship Research and Development Center
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