142 



0.02 0.04 0.06 0.08 0.10 0.02 



r u'^/u . Vt:-^/u , K™/u , -u-vvu ^ 



o o ' o o 



FIGURE 15. Measured distributions of Reynolds stresses for afterbody 2. 



V^/u . K^u , K^/u , Z^i^ 2 



1 ^ ^ I r 



AFTERBODY 2 



0.12 



-u V 

 _2 







O <^ 



b L_ 



FIGURE 16. Measured distribu- 

 tions of turbulent structure 

 parameter. 





X/L X/L 



0.840 O <"55 



^ 0.934 □ 0.846 



[7 0.970 ^ 0.934 



(^ 0.977 /^ 0.964 



Q 1.0076 



O 1.057 



(^ 1.182 



\7 



D 

 Q 



O 



o 





0.6 0.8 



r — r 



iD 



-X>J 



