. Drag, flow transition, and laminar separation on nine bodies of revolution having different forebody shapes. Drag (Aerodynamics); Turbulent boundary layer; Submarines (Ships). — — — — Figure 14 — Measured Total Drag Coefficients of Models 1 through 9 1 1 1 1 1 1 1 • BARE HULL A WIRE xk/D = O x,/D = Figure 14a - Model 1 4' 1 1 1 1 1 • BARE HULL ? A O I I I I I xk/D = xk/D = xk/D = I - I f< • 4 I 10 15 20 25 30 35 40 v-6 RL- 10~ Figure 14b - Model 2 40. Pleas


. Drag, flow transition, and laminar separation on nine bodies of revolution having different forebody shapes. Drag (Aerodynamics); Turbulent boundary layer; Submarines (Ships). — — — — Figure 14 — Measured Total Drag Coefficients of Models 1 through 9 1 1 1 1 1 1 1 • BARE HULL A WIRE xk/D = O x,/D = Figure 14a - Model 1 4' 1 1 1 1 1 • BARE HULL ? A O I I I I I xk/D = xk/D = xk/D = I - I f< • 4 I 10 15 20 25 30 35 40 v-6 RL- 10~ Figure 14b - Model 2 40. 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 Power, John L; David W. Taylor Naval Ship Research and Development Center. Bethesda, Md. : David W. Taylor Naval Ship Research and Devlopment Center


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