Test Case 1.4


KVLCC2M [Geometry ]

Conditions

Froude number ( Fn ) Reynolds number ( Rn )
0 3.945×106

Items and Remarks

Figure Number Items Remarks
  Integral variables:
Coefficients of
   total resistance (CT), split into
   pressure (CP) and
   friction (CF) components
and Uncertainty analysis( USN, UV, E )
Experimental results are available
Table( NMRI )

UD = 0.7 [%CT]

Fig. 1.4-1 Axial velocity contours and cross flow
vectors on the propeller plane (x/Lpp=0.48)
 
Fig. 1.4-2 Velocity on the propeller plane
(x/Lpp=0.48) at z/Lpp=-0.05
To be compared with experimental results
download ( NMRI )
Fig. 1.4-3 Uncertainty analysis of the above item UD = 0.5, 1.0, 1.0 for u, v. w [%U] along the entire cut (proceedings of CFD Wordshop 2000)
Fig. 1.4-4 Kinematic eddy viscosity ( νt ) and longitudinal component of vorticity ( ω x ) contours on the propeller plane   (x / LPP = 0.48)  
Fig. 1.4-5 Hull surface pressure contours ( port side view )  
Fig. 1.4-6 Hull surface pressure contours ( back view )  
Fig. 1.4-7 Hull surface pressure contours ( bottom view )  
Fig. 1.4-8 Limiting streamlines ( port side view )