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 = 0.704, 0.831, 0.873 



15 



