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EFD > Validation data >
Series 60 propeller hull interaction
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Experiment
Results
are presented from a towing-tank experiment of propeller-hull interaction
conducted in order to provide detailed documentation of the complete flow
field appropriate both for explicating the flow physics and validating
computational methods. Mean-velocity and pressure field measurements
were made for the with- and without-propeller conditions for the Series 60
CB=0.6 hull form at numerous stations both upstream and downstream of the
propeller and in the near wake region. Surface-pressure
distributions and wave profiles were measured for both conditions.
Resistance and self-propulsion tests were also 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 flow with and without propeller. The results are
analyzed to assess the nature of the interaction between the propeller and
the hull boundary layer and wake. To this end, use is made of a
propeller-performance program with both nominal and effective
inflows. It is shown that most features of the interaction can be
explained as a direct consequence of the propeller loading resulting from
its operation with a three-dimensional nonuniform inflow.
Data, equipment, and conditions
|
Data |
Equipment |
Fr |
KT,
KQ, J |
Locations |
|
Resistance |
Dynamometer |
0.08-0.27 |
- |
- |
|
Propeller open water |
Dynamometer |
0.10-0.36 |
- |
- |
|
Self propulsion |
Dynamometer |
0.08-0.27 |
- |
- |
|
Wave profiles |
35 mm camera |
0.16, 0.25, 0.30, 0.35 |
- |
|
|
Surface pressure |
Pressure transducers |
0.16 |
0.234, 0.0411, 0.654 |
|
|
Boundary layer and wake flow
field |
5-hole pitot probe and
pressure transducers |
0.16 |
0.234, 0.0411, 0.654 |
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 |
|


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Sample photo
Sample data
Surface pressures (Cp) at
x = 0.95 (red), x = 0.9625 (green), and x = 0.975 (blue) for the
with-propeller condition
Crossflow vectors (V, W) at
x = 0.95 for the
with-propeller condition


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References
Toda, Y., Stern, F., Tanaka, I., and Patel, V.C., (1988),
"Mean-flow measurements in the boundary layer and wake of a Series 60 CB=0.6 model
ship with and without propeller," IIHR Report No. 326, 100 pp.
Toda, Y., Stern, F., Tanaka, I., and Patel,
V.C.,
(1988), "Mean-flow measurements in the boundary layer and wake of a Series 60 CB=0.6
model ship with and without propeller," J. Ship Research, Vol. 34, No.
4, pp. 225-252.
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This page last updated:
01/24/2006 07:58:19 AM |