1.  All figures shall be submitted as Postscript (*.ps or *.eps) files.  

2.  As shown in example figures, please include indentifier provided by workshop organizers.

3.  Integral values shall be submitted as ASCII file.

4.  Transfer all files to IIHR anonymous ftp server

1. connect to ftp.iihr.uiowa.edu
   login:  anonymous
   password:  your email address
2. change directory to /incoming/iihr/g2k
3. make a directory for yourself using either your last name or institution as the directory name
4. put all of your files in this directory
5. notify Dr. Volker Bertram (email: Bertram@hsva.de) that your submission is on the ftp server.

Items for Model-Scale KVLCC2 comparisons & validation:

Table 1.  Integral variables:  CT, CF, Cp, k

Filename	kvlcc2_iv_ms.ascii
Example tables	Comparison

Figure 1.  Velocity field contours and cross-plane vectors at propeller plane

Filename	kvlcc2_vel1_ms.eps
Axis size	120mm x 40mm
Horizontal-axis variable and range
Vertical-axis variable and range
Reference vector	magnitude = 0.1 corresponds to 2mm
Contour range and levels
Style	U contours left side; V-W vectors right side
Example image

Figure 2.  Axial velocity in propeller plane along z/L=-0.05, comparison to EFD data.

Filename	kvlcc2_vel2_ms.eps
Axis size	80mm x 60mm
Horizontal-axis variable and range
Vertical-axis variable and range
Style	CFD solid line;  EFD open circles
Example image

Figure 3.  Axial velocity in propeller plane along z/L=-0.05, validation.

Filename	kvlcc2_vel3_ms.eps
Axis size	80mm x 60mm
Horizontal-axis variable and range
Vertical-axis variable and range
Validation scale	Ship speed, U
Style	E solid line;  +/- Uv dashed line
Example image

NOTES
1.  Comparison Error, E=D-S, where D is the data value, and S is the simulation value.  E% is obtained by normalizing by validation scale, i.e., E%=(D-S)/(validation scale)*100

2.  U_V = sqrt(U_D²+U_SN²) is the validation uncertainty [see equation 33 of  Stern et al. (1999)]

3.  U_D is the data uncertainty.

4.  U_SN is the simulation numerical uncertainty [see equation 8 of Stern et al. (1999)]

Figure 4.  Turbulent kinetic energy and pressure field contours at propeller plane

Filename	kvlcc2_ke1_ms.eps
Axis size	120mm x 40mm
Horizontal-axis variable and range
Vertical-axis variable and range
Contour range and levels
Style	k contours left side; Cp contours right side
Example image

Figure 5.  Turbulent kinetic energy in propeller plane along z/L=-0.05, comparison to EFD data.

Filename	kvlcc2_ke2_ms.eps
Axis size	80mm x 60mm
Horizontal-axis variable and range
Vertical-axis variable and range
Style	CFD solid line;  EFD open circles
Example image

Figure 6.  Turbulent kinetic energy in propeller plane along z/L=-0.05, validation.

Filename	kvlcc2_ke3_ms.eps
Axis size	80mm x 60mm
Horizontal-axis variable and range
Vertical-axis variable and range
Validation scale	range of k, (kmax-kmin) = 20
Style	E solid line;  +/- Uv dashed line
Example image

NOTES
1.  Comparison Error, E=D-S, where D is the data value, and S is the simulation value.  E% is obtained by normalizing by validation scale, i.e., E%=(D-S)/(validation scale)*100

2.  U_V = sqrt(U_D²+U_SN²) is the validation uncertainty [see equation 33 of  Stern et al. (1999)]

3.  U_D is the data uncertainty.

4.  U_SN is the simulation numerical uncertainty [see equation 8 of Stern et al. (1999)]

Figure 7.  Hull surface-pressure contours, side view.

Filename	kvlcc2_pr1_ms.eps
Axis size	125mm x 35mm
Horizontal-axis variable and range
Vertical-axis variable and range
Contour range and levels
Style	(+) solid lines; (-) dashed lines
Example image	Not available yet

Figure 8.  Hull surface-pressure contours, aft view.

Filename	kvlcc2_pr2_ms.eps
Axis size	75mm x 50mm
Horizontal-axis variable and range
Vertical-axis variable and range
Contour range and levels
Style	(+) solid lines; (-) dashed lines
Example image	Not available yet

Figure 8.  Limiting streamlines, side view

Filename	kvlcc2_ls1_ms.eps
Axis size	125mm x 35mm
Horizontal-axis variable and range
Vertical-axis variable and range
Style	Participants choose starting points and spacing
Example image

Items for Full-Scale KVLCC2 comparisons:

Table 2.  Integral variables:  CT, CF, Cp, k

Filename	kvlcc2_iv_fs.ascii
Example tables	Comparison

Figure 9.  Velocity field contours and cross-plane vectors at propeller plane

Filename	kvlcc2_vel1_fs.eps
Axis size	75mm x 30mm
Horizontal-axis variable and range
Vertical-axis variable and range
Referemce vector	magnitude = 0.1 corresponds to 2mm
Contour range and levels
Style	U contours left side; V-W vectors right side
Example image

Figure 10.  Turbulent kinetic energy and pressure field contours at propeller plane

Filename	kvlcc2_ke1_fs.eps
Axis size	75mm x 30mm
Horizontal-axis variable and range
Vertical-axis variable and range
Referemce vector	magnitude = 0.1 corresponds to 2mm
Contour range and levels
Style	U contours left side; V-W vectors right side
Example image

Figure 11.  Hull surface-pressure contours, side view.

Filename	kvlcc2_pr1_fs.eps
Axis size	125mm x 35mm
Horizontal-axis variable and range
Vertical-axis variable and range
Contour range and levels
Style	(+) solid lines; (-) dashed lines
Example image	Not available yet

Figure 12.  Hull surface-pressure contours, aft view.

Filename	kvlcc2_pr2_fs.eps
Axis size	75mm x 50mm
Horizontal-axis variable and range
Vertical-axis variable and range
Contour range and levels
Style	(+) solid lines; (-) dashed lines
Example image	Not available yet

Figure 13.  Limiting streamlines, side view

Filename	kvlcc2_ls1_fs.eps
Axis size	125mm x 35mm
Horizontal-axis variable and range
Vertical-axis variable and range
Style	Participants choose starting points and spacing
Example image