|
EFD > Validation data >
Series 60 steady flow
|
Experiment
Results
are presented from a towing-tank experiment conducted in order to
explicate the influence of wavemaking by a surface-piercing body on its
boundary layer and wake and provide detailed documentation of the complete
flow field appropriate for validating computational fluid dynamics
methods.
Mean velocity and pressure field measurements were
performed for two Froude numbers, 0.16 and 0.316, for the L=3.048-m Series
60 CB=0.6 hull form at numerous stations from bow to stern and into the
near wake. For Froude number=0.316, free surface effects are very
significant, whereas for Froude number=0.16, they are negligible, except
near the bow, such that comparison of the results enables the
identification of the salient features of the wave-induced effects.
Wave profiles and nearfield and farfield wave elevations were also
measured. In addition, resistance tests were conducted. In the
references below, the experimental equipment and procedures are described
and the results are discussed to point out the essential differences
between the flows at low and high Froude number. On the forebody,
the differences are primarily in the outer (inviscid) flow, except at the
bow, whereas on the afterbody and in the near wake, both the inner
(viscous) and outer flows are altered. Most of the interaction
between wavemaking and the boundary layer and wake can be explicated as a
result of the wave elevations, wave-induced pressure gradients, and the
displacement effects of the boundary layer.
Data, equipment, and conditions
|
Data |
Equipment |
Fr |
Locations |
|
Resistance |
20 kg loadcell |
0.1-0.36 |
- |
|
Wave profiles |
35 mm camera |
0.25, 0.3, 0.316 |
|
|
Far field wave elevations |
Capacitance wires |
0.316 |
|
|
Near field wave elevations |
Servo-type wave gage |
0.316 |
|
|
Boundary layer and wake flow
field |
5-hole pitot probe and
pressure transducers |
0.16, 0.316 |
x / L
= 0, 0.1, 0.2, 0.4, 0.6,
0.8, 0.9, 1.0, 1.1, 1.2,
y / L
= 0-0.03,
z / L
= -0.125-0 |
|
 |
Sample data
Flow field contours of axial
velocity U at x = 0, 0.1, 0.2, 0.4, 0.6, 0.8, 0.9,
1.0, 1.1, 1.2 (foreground) and wave field contours (background)
for the Series 60 CB = 0.6 at Fr =
0.316.


^^^ Click here to get WinZip ^^^ |
|
References
Longo, J., (1990), "Scale Effects on Near-Field Wave Patterns,"
M.S. thesis, Department of Mechanical Engineering, The University of Iowa, Iowa City, IA.,
141 pp.
Longo, J., Stern, F., and Toda, Y., (1993),
"Mean-Flow Measurements in the Boundary Layer and Wake and Wave Field of a Series 60
CB=0.60 Ship Model - Part 2: Scale Effects on Near-Field Wave Patterns and Comparisons
with Inviscid Theory," Journal of Ship Research, Vol. 37, No. 1, pp. 16-24.
Toda, Y., Stern, F., and Longo, J., (1991), "Mean-Flow
Measurements in the Boundary Layer and Wake and Wave Field of a Series 60 CB=0.6 Ship
Model for Froude Numbers 0.16 and 0.316," IIHR Report No. 352, 188 pp.
Toda, Y., Stern, F., and Longo, J., (1992),
"Mean-Flow Measurements in the Boundary Layer and Wake and Wave Field of a Series 60
CB=0.6 Ship Model - Part 1: Froude Numbers 0.16 and 0.316," J. of Ship
Research, Vol. 36, No. 4, pp. 360-377.
<<<Click here to get Adobe Acrobat |

This website is powered
by:

Comments or questions:
email to frederick-stern@uiowa.edu
Copyright © The University of
Iowa 2005.
All rights reserved.
This page last updated:
01/24/2006 07:58:01 AM |