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Thrusters Numerical Analysis of Flow Around a Thruster Norbert W. H. Bulten Wärtsilä Propulson, Netherlands October 17-18, 2006 Return to Session Directory

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Page 1: Thrusters Numerical Analysis of Flow Around a …dynamic-positioning.com/proceedings/dp2006/thrusters_bulten_pp.pdfThrusters Numerical Analysis of Flow Around a Thruster ... Formula

Thrusters

Numerical Analysis of Flow Around a Thruster

Norbert W. H. Bulten

Wärtsilä Propulson, Netherlands

October 17-18, 2006

Return to Session Directory

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© Wärtsilä

Norbert Bulten18 October 2006

Numerical Analysis of Flow around a Thruster

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� General introduction about thrusters� Application of nozzles� Performance predictions issues

� Research method: CFD� State-of-art numerical techniques� Experience at Wartsila with CFD� Basic priciples of CFD

� Results of analyses� Propeller-HR-nozzle configuration� Complete thruster-unit

� Conclusions

Topics

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General thruster introduction

� Thrusters are applied for:� Dynamic positioning� Heavy lift vessels� Offshore support vessels� Cable laying vessels� Tugs

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General thruster introduction

� Thrusters can be equipped with or without nozzle

Lips HR-nozzle

Open propeller

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Application of nozzles

� Nozzles are applied to increase thrust at low ship speed. Typical examples of low speed operation are:

� Bollard pull � Dynamic positioning� Fishing� Heavy lift vessels

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Application of nozzles

� Basic principle of nozzle: section acts similar as wing section

� Pressure distribution around nozzle changes due to propeller action

Additional thrust

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Typical nozzle types

� Cross-sectional profile of nozzles:

� 19A� 37� LIPS-HR

� Full scale measurements show 8% bollard pull improvement for HR compared to 19A

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Performance prediction of nozzles

� In general, open propeller performance is based on model scale experiments.

� Full scale performance is based on measured data in combination with scaling methods (ITTC’78)

� Scaling of ducted propellers (=propeller + nozzle configuration) not well understood

� New nozzle designs, like Lips HR-nozzle, do not behave like old 19A nozzles.

� Advanced numerical method (CFD) is applied to predict full scale performance of propeller with HR-nozzle

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Performance prediction of thrusters

� Conventional thruster performance is based on model scale measurements.

� Scaling of thruster performance is more complex than ducted propeller, due to strut and thruster house

� Full scale performance of thruster unit can be based directly on state-of-the-art numerical calculations.

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Introduction to CFD

� CFD = Computational Fluid Dynamics

� State-of-the-Art numerical method to calculate flow field in three-dimensions

� Velocity� Pressure distributions

� Method takes scaling effects into account

� Applications in industry:� Formula 1� Marine� Oil and gas� ….� …

Fire and smoke dispersion

(www.cd-adapco.com)

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Examples of CFD results

� Experience at Wartsila Propulsion with CFD� Propellers� Thrusters� Waterjets� Propeller – hull interaction

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Basic principles of CFD

� Definition of numerical domain around geometry of interest (for example thruster unit)

� Numerical domain is split in large number of small cells -> grid or mesh with about 1.000.000 cells

� Velocity and pressure are solved in each cell

� Results of velocity field and pressure distribution are analyzed. This provides among others forces on the thruster:

� Propeller thrust� Nozzle thrust� Resistance of thruster house

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Results of HR-nozzle analyses

� Comparison of model scale and full-scale calculations

� Open water efficiency is not suitable for bollard pull analysis

� Merit coefficient is used instead:

� Results for Ka5-75 propeller show 9% increase

q

tt

K

K

mc

23

0

0.2

0.4

0.6

0.8

1

1.2

1.4

1.6

model scale full scale

" "

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Results of thruster-unit analyses

� Pressure distribution along thruster unit

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Results of thruster-unit analyses

� Thrust and resistance of thruster-unit is analyzed for all parts separately:

propeller

nozzle

gearhouse

strut

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Drag of thruster house

� Resistance of thruster house is present at low J values

Resistance of thruster house

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

J [-]

Dra

g c

oef

fici

ent

bas

ed o

n p

rop

elle

r R

PM

an

d d

iam

eter

Kd_tot

Kd_house

Kd_strut

Curve-fit_overall

Curve_fit-house

Curve-fit-strut0

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Conclusions

� Bollard pull performance of HR-nozzle at full scale is significantly better than on model scale

� Drag of a thruster-house is present both at low ship speed and high ship speed. Though, the cause is different.

� The state-of-the-art numerical method of CFD is suitable to predict the full scale performance of ducted propellers and complete thruster units.