Research Projects
Viscous flow about under water bodies
The motivation for this project relates to the hydrodynamic design of remotely
operated underwater vehicles (ROVs) currently used for mine disposal and being
investigated for force multiplication with submarines. They are typically low aspect
bluff bodies operated at a range of Reynolds numbers and incidences for which a range
of flow regimes are possible. These include attached and separated flows ranging from
sub to super-critical at low and high incidence. The objectives of this project are
experimental investigation of the flows described as well as the gathering of
experimental data sets for comparison with computational fluid dynamics (CFD). Two
physical models, an ellipsoid and a spheroid, have been developed for sting mounting in
the cavitation tunnel and include instrumentation for measurement of surface flow
properties. The models have also been developed for sting mounting on a 6 component
force balance or for force measurement with an internal 6 component force balance.
Studies of off body flow phenomena are being carried out using a range of physical
probes and an automated 3 component traverse system. This project is supported by the
Australian Maritime College, the Maritime Platforms Division of the Defence Science and
Technology Organisation and the University of Tasmania.
Project supervisors:Dr Paul Brandner (AMC) and Dr Greg Walker
(UTas)
DSTO researcher/PhD Student:Mr David Clarke (MPD - DSTO)
Investigation of Spheroid Boundary Layer Transition Using Sting Mount and 3D
Automatic Traverse and 1D Fast Response Probe
Flow Visualisation of Separation on a Spheroid
Ventilated super-cavitating ride control foils
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Test of a Super-cavitating Ventilated Hydrofoil
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This project involves research and development contributing to the realisation of a
patented system for, among other applications, ride control foils for high speed craft.
The patented system developed by Elms Australia, as applied to ride control, consists
of a flapped symmetric hydrofoil arrangement that can be used for generation of
bi-directional lift. The flap is configured to produce a forward facing step or
interceptor upon upward or downward deflection. This combined with ventilation produces
a simple means to generate lift in an upward or downward direction suitable for high
speed operation. The problem of ride control for high speed craft involves the use of
lift producing devices at low cavitation numbers and there are several advantages if
these can be made to operate in the supercavitating flow regime including flow
stability and improved efficiency. A range of basic experimental and numerical
investigations are being made to study viscous effects with natural and ventilated
cavities associated with interceptors. The results of these are being used in the
design of suitable foil sections to be tested in the cavitation tunnel. Foil tests
include both static and dynamic test using an oscillating 6 component force balance. It
is also envisaged that as part of the project results from foil investigations will be
developed in other applications such as high speed propulsors. This project is
supported by the Australian Maritime College and Elms Australia.
Project supervisors:Dr Paul Brandner (AMC) and Mr Tony Elms (Elms
Australia)
PhD Student:Mr Bryce Pearce (AMC)
2D Boundary Element Solution for Super-cavitating Flow Behind a Hydrofoil With
Trailing Edge Fence or Inteceptor
Performance of surfboard fins
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Testing of a Surfboard Fin
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The development of surfboards, and fins for their control, has to date been purely
based on surfer and manufacturer experience or current trends. With ever increasing
competitiveness in professional and amateur surfing Surf Hardware International, (SHI),
an international manufacturer of surfboard accessories including fins, decided upon a
research and development program for their range of surfboard fins. The project is
headed by Americas Cup yacht designer, Mr Andrew Dovell of Murray, Burns and Dovell
with research and testing expertise being contributed by cavitation tunnel staff. The
existing range of ISH fins have been tested in the cavitation tunnel using a 6
component force balance as well as flow visualisation studies for investigation of
viscous and cavitation aspects. Tests are also being carried out on a range of new fin
designs utilising modern foil sections and current knowledge on planforms to develop a
series of fins optimised for various Reynolds numbers and incidences. This project is
funded by International Surf Hardware and by the AusIndustry R&D Start Program.
Flow investigation about submarine counter measures
Counter measures are a critical aspect of submarine defence and to better understand
their behaviour hydrodynamic manoeuvring models are being developed for trajectory
prediction after ejection. The hydrodynamic forces acting on the counter measure
required for the mathematical modeling are being investigated in the cavitation tunnel.
A range of models with differing scales, configurations and incidence are being tested
using a 6 component force balance in both cavitating and non-cavitating conditions.
This project is supported by the Australian Maritime College, the Maritime Platforms
Division of the Defence Science and Technology Organisation and the University of
Tasmania.
Researchers:Dr Paul Brandner (AMC), Mr David Clarke (MPD - DSTO), Mr
Brendon Anderson (MPD - DSTO) and Dr Greg Walker (UTas).
Flow friction due to bio-fouling
AMC researchers are working in collaboration as part of a larger UTAS project
involving the biological and hydrodynamic investigation of bio-fouling in hydroelectric
power schemes. The presence of biological growth increases the cost of maintenance and
reduces operating efficiency of hydroelectric infrastructure. UTas researchers are
investigating the biological, topographical and hydrodynamic aspects of the fouling.
Cavitation tunnel researchers are involved with the development of instrumentation and
investigation of skin friction associated with the bio-fouling. The drag of plates with
equivalent roughness and the actual bio-fouling are being measured in UTas and AMC
facilities as well as investigation of boundary layers associated with the fouling. A
new 1 dimensional balance is being developed for use in the AMC towing tank and
cavitation tunnel as well as instrumentation for a new flume at UTas which will contain
the organisms cultured from field samples. This project is funded by a UTas Australian
Research Council Linkage Grant.
Unsteady and hydro-elastic performance of propellers
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Propeller Cavitation
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Propeller performance in high speed and naval applications is an area of ongoing
investigation. Within this project new experimental and numerical methods for the study
of a range of performance aspects are being developed. A new `silent' propeller
dynamometer is being designed for acoustic measurements associated with submarine
propulsion studies. New methods for simulation of wakes using vortex generators and
injection of waterjets are being investigated. To better investigate simulated wakes
for propulsion studies a 3D fast response probe and 3D automatic traverse have been
recently completed. Using this system the intention is to not only investigate the
effects of the mean velocity distribution but also the turbulence distribution on
cavitation inception and unsteady non-cavitating and cavitating propeller performance.
Experimental investigations also contribute to the development of Reynolds Averaged
Navier Stokes Solvers for propeller performance prediction. This project is supported
by the Australian Maritime College, the Maritime Platforms Division of the Defence
Science and Technology Organisation and the University of Tasmania
Flow investigation about submarine control surfaces and other
appendages
The performance of a submarine depends fundamentally on flow quality about the hull,
appendages and control surfaces and a range of basic studies are being made to
investigate means of improvement. These include experimental and numerical
investigations of turbulent flow, boundary layer instabilities, skin friction, corner
flows and fluid structure interactions. This project is supported by the Australian
Maritime College, the Maritime Platforms Division of the Defence Science and Technology
Organisation, the University of Tasmania and the Defence Materiel Organisation.
Waterjet propulsor performance
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Waterjet Inlet Lip Cavitation
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Waterjets have become the standard propulsion system for large high speed craft and
whilst these have shown to be successful there remains considerable scope for design
improvement through greater understanding of waterjet flows and optimisation. Flow
problems, with flush type inlet ducts, relate to ingestion of the hull boundary layer
and the complex viscous flow within the inlet streamtube and duct. These problems are
manifested in the occurrence of cavitation, flow separation, unsteady flow, flow
non-uniformity at the pump face and possible vibration. Investigations to date have
focused on the inlet flow since flow problems associated with the pump relate largely
to those created by the inlet. A range of instrumentation and experimental equipment
has been developed for inlet duct flow investigation as well as for data set collection
for comparison with computational predictions. These include methods for simulation of
the hull boundary layer upstream of the inlet, probes for flow field surveys within the
duct and at the notional pump face and techniques for flow visualisation including
cavitation. The use of flow manipulation devices within the duct for elimination of
separation and improvement of pump face uniformity have also been successfully
investigated experimentally and using computational models. Computational models for
prediction of tunnel blockage, optimisation and to aid in diagnosing flow problems are
being developed in parallel with the experimental program. This project follows on from
earlier extensive wind tunnel investigation of waterjet inlet duct flows by UTas. This
project is supported by the Australian Maritime College and the University of
Tasmania/Tasmanian Partnership for advanced Computing.
Researchers:Dr Paul Brandner (AMC), Dr Greg Walker and Dr Jason
Roberts (UTas/TPAC).
Schematic of a Waterjet Propulsor
Flow Issues Associated with Waterjet Propulsors