. Boundary-layer flow on an axisymmetric body with an inflected stern. Turbulent boundary layer. Figure 6 - Computed and Measured Static Pressure Distributions Across Stern Boundary Layer of Afterbody 5 T 1 1 1 r. -1 1 r- -1 1 1 1 1 1 1 1 1 1 r THEORY: DISPLACEMENT BODY ACTUAL BODY EXPERIMENTS: OPEN SYMBOLS - OFF BODY POINTS SOLID SYMBOLS - ON BODY POINTS /////LOCATION OF DISPLACEMENT SURFACE Figure 6a - Nondimensional Axial Lengths, x/L = , , 15. Please note that these images are extracted from scanned page images that may have been digitally enhanced for readability - colorat
. Boundary-layer flow on an axisymmetric body with an inflected stern. Turbulent boundary layer. Figure 6 - Computed and Measured Static Pressure Distributions Across Stern Boundary Layer of Afterbody 5 T 1 1 1 r. -1 1 r- -1 1 1 1 1 1 1 1 1 1 r THEORY: DISPLACEMENT BODY ACTUAL BODY EXPERIMENTS: OPEN SYMBOLS - OFF BODY POINTS SOLID SYMBOLS - ON BODY POINTS /////LOCATION OF DISPLACEMENT SURFACE Figure 6a - Nondimensional Axial Lengths, x/L = , , 15. 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 Huang, T. T. (Thomas T. ); Groves, Nancy C; Belt, Garnell S; David W. Taylor Naval Ship Research and Development Center. Bethesda, Md. : David W. Taylor Naval Ship Research and Development Center
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