E. J. Richards, J. L. Willis, and D. J. M. Williams 297 
Transducer 
2:0 
0°5 
Distance from nose 
Fig. 15.20. Suggested shape for submarine nose: (a) nose shape; (b) velocity 
distribution. 
fo) ot 02 o3 o4 os 06 o7 os x 
Fig. 15.21. Velocity distribution of thirty-per-cent-suction wing with tail fore- 
most; six degrees incidence. 
