244
(WED) and Bertram, 1998) or 7‐9% from a
combination of wake equalising duct and pre‐swirl
fins (Mewis, 2008, Mewis, 2009). In general, the
negative aspects of the devices include the
considerablecostofinstallation,andalsothereported
reluctanceofmanufacturerstoguaranteetheclaimed
savings.
The claims
may not give details as to the
conditions under which the savings have been
achieved and/or how the savings have been
calculated and/or measured. Furthermore, the
magnitude of the savings may well be within the
rangeofuncertaintiesandmeasurementerrorsonthe
full‐scale vessel. Consequently, cautious operators
may
wellbeskepticalaboutthevalidityofthefigures
being presented to the market, and it is absolutely
reasonable and necessary for a buyer to verify
independently the amount of savings before any
investmentonanESDorESDs.
InanycaseforinstancetheWED devicemust be
customizedto
fittotheafterbodyoftheshipinterms
ofperformingitssupposedfunction.TheDesigneris
therefore placed in the front of multiple geometric
solutionsfrombetweenhehastomakeachoice.This
paper is intended to help the Designers to have a
rationalchoosingapproachbyinvolving
thenumeric
optimizationofthegeometryoftheWEDinorderto
selectthebestfittedWEDtoperformthebestinorder
toachievesomepredefinedparameters.
2 CADANDFINITEVOLUMEANALISYS(FVA)
MODELOFTHESHIP
The goal of this paper is to calculate via software
Ansys 13
TM
the best geometric solution for a WED
device.ItisknownthatapoordesignoftheWEDis
notonlyimprovingtheoverallefficiencyofthevessel
butmayhaveanadverseimpactfailingtoachieveits
purpose.
The model has as departure point a real
portcontainer as seen below,
with the following
parameters(Fig.1):
LengthL‐[m]‐173
BreadthB‐[m]‐25
DraughtT‐[m]‐9.50
DiameterD‐[m]‐5
NumberofbladesZ‐6
PropellerRPM‐120
AverageSpeed‐16knots(7m/s)
Figure1.Port‐Container
Inordertohaveastartingpointforthesimulation,
first of all the afterbody was firstly CAD generated
withtheWEDdeviceattached,andalltheparameters
for fluid flow were calculated accordingly.From
thatpoint,theAnsysDesignExplorerwasinvolvedin
ordertooptimizethegeometry(Fig.2).
Figure2.CADgeometrywithWED
Inordertoprovidemoredetailsonthegeometry
of starting model of the WED device and the
optimization input parameters, the below figure is
shown,withdimensionsin[mm](Fig.3):
Figure3.WEDdevicegeometry
5 input geometric parameters were defined as
follows(Table1):
Table1.Inputgeometricparameters
_______________________________________________
Name TypeLowerlimit Upperlimit
_______________________________________________
P1 Angle Continuos 14[grade] 22[grade]
Minimize
P2 DuctLength Continuos 1980[mm] 2420[mm]
Minimize
P3 Smallradius Continuos 1600[mm] 2250[mm]
Minimize
P4 BiggerconeContinuos 2250[mm] 2750[mm]
radius
Minimize
P5 Distancefromthepropeller
Continuos 1800[mm] 2200[mm]
Minimize
_______________________________________________