comunicaÇÃo tÉcnica - ipt · 2018. 6. 22. · the use of cfd on the naval engineering research...
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COMUNICAÇÃO TÉCNICA ______________________________________________________________________________________________________________________________________________________________________________________________________
Nº175344
The use of CFD on the Naval Engineering Research at IPT
João Lucas Dozzi Dantas
Palestra apresentada no SIMCETER USERS MEETING SOUTH AMERICA, 2018, São Paulo A série “Comunicação Técnica” compreende trabalhos elaborados por técnicos do IPT, apresentados em eventos, publicados em revistas especializadas ou quando seu conteúdo apresentar relevância pública. ___________________________________________________________________________________________________
Instituto de Pesquisas Tecnológicas do Estado de São Paulo S/A - IPT
Av. Prof. Almeida Prado, 532 | Cidade Universitária ou Caixa Postal 0141 | CEP 01064-970
São Paulo | SP | Brasil | CEP 05508-901 Tel 11 3767 4374/4000 | Fax 11 3767-4099
www.ipt.br
The use of CFD on the Naval
Engineering Research at IPT
IPT – Institute for Technological Research
João Lucas Dozzi Dantas – [email protected]
Agenda: About IPT – Institute for Technological Research
Vessel Resistance and Motion
Geometry simplification using porous approach
Propeller blockage and hydrophobic investigation
Laminar-turbulent transition model
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IPT – Institute for Technological Research
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IPT – Institute for Technological Research
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IPT-NAVAL: Towing Tank
Large Section: 200 x 6.6 x 4.5 m
Narrow Section: 60 x 3.7 x 2.0 m
Maximum test speed: 3.5 m/s
Model length: up to 6.0 m
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IPT-NAVAL: Cavitation Tunnel
Section test: 0.5 x 0.5 m²
Range of pressure: 0.2 ~ 1.6 atm
Propeller rotation: up to 3000 rpm
Advance velocity: up to 5.0 m/s
IPT’s Cavitation Tunnel, model Kempf & Remmers K18, was inaugurated in 1963 in a
partnership with Brazilian navy
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IPT-NAVAL: Cavitation Tunnel: Instrumentation Capabilities
Force, torque and vibration
measurement
• Strain gauges and load cells
Strobe light
Velocity measurements
• Pitot
• Acoustic (ADV)
• Laser (PIV and LDV)
Measurement of dissolved oxygen
Underwater acoustic sensors
Vessel Resistance
and Motion Some results published in:
PELICIA, R.S.; DANTAS, J.L.D. Model Calm Water Resistance and Motion – Simulation, Experiments and Verification.The
30th American Towing Tank Conference. SNAME. 2017.
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Vessel Resistance and Motion
Objectives
Calm water resistance test are common test in towing tanks, being
used to verify a hull performance or calibrate a numerical model.
• Verify the numerical model through mesh sensitiveness analysis
• Validate the numerical model by comparison of towing tank results
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Case study
Two platform supply vessel model
Prototype planform:
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Results: Resistance
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Results: Wave incidence
Only M536 (Prototype I)
Draft of 6.6 m
Vp =1.048 m/s (15 knot)
Some results published in:
KATSUNO, E.T.; CASTRO, F.S.; DANTAS, J.L.D. Debris Containment Grid CFD validation with Towing Tank
Tests.The 30th American Towing Tank Conference. SNAME. 2017.
KATSUNO, E.T.; CASTRO, F.S.; DANTAS, J.L.D. Hydrodynamic Analysis of Debris Containment Grid in
Hydropower Plant Using Porous Media.24th International Congress of Mechanical Engineering. ABCM. 2017.
KATSUNO, E.T.; GOMES, G.G.; CASTRO, F.S.; DANTAS, J.L.D. Numerical Analysis of Debris Containment Grid
Fluid-Body Interaction.37th International Conference on Ocean, Offshore and Artic Engineering. ASME. 2018.
Simplification of a floating line
using porous approach
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Objectives
Develop a simplified numerical model of a truncated version (with fewer modules)
of a debris containment grid line
• Dynamic Fluid Body Interaction - DFBI
• Several conditions: Advance velocity and side-slip angle
Hydrodynamic Investigation is conducted using CFD software
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Methodology
Complete representation Simplified
representation using
porous media approach
Line with simplified
representation
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Complete representation setup
Two DoF: sinkage of the module and rotation of the chassis
Two regions: domain region (include the grid) and chassis region
Boundary conditions of domain region
Boundary conditions of
chassis region
Log boom module:
Grid + chassis
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Simplified representation setup
Dimensions are the same as complete representation.
Grid are simplified by a porous region
Fewer elements
Boundary Conditions of Domain (I), Grid (II), Chassis (III) and Frontal part of Chassis (IV) regions (figures
are not in the same scale)
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Porous formulation
Comparative of complete and porous model in grid force magnitude (x and y directions)
(left); and in moment (right)
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Log Boom line
Six simplified representation
• 13 regions with overset interfaces
Float-Grid
Grid-Grid
Edges
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Next steps
Modeling porous region using Momentum source
Increase number os lof boom modules
Compare results with experimental values obtained in IPT’s Towing Tank
Some results published in:
KATSUNO, E.T.; DANTAS, J.L.D. Investigação da metodologia para simulações de propulsores utilizando fluidodinâmica
computacional. 26º Congresso Nacional de Transporte Aquaviário, Construção Naval e Offshore. SOBENA. 2016.
KATSUNO, E.T.; DANTAS, J.L.D. Analysis of the Blockage Effect on a Cavitation Tunnel using CFD Tools. 36th
International Conference on Ocean, Offshore and Artic Engineering. ASME. 2017.
KATSUNO, E.T.; DANTAS, J.L.D.; SILVA, E.C.N. Analysis of Hydrophobic Painting in Model-Scale propeller. 37th
International Conference on Ocean, Offshore and Artic Engineering. ASME. 2018.
Propeller blockage and
hydrophobic investigation
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CFD model study
Domain size study
V&V study
Mesh topology study
Turbulence model
Nu
mb
er
of e
lem
en
ts
Trimmed Polyhedral
Model KT KQ 𝜼
Experimental 0,330 0,0433 0,231
SA 0,317 0,0419 0,256
SST 0,316 0,0417 0,256
SST LowRe 0,316 0,0418 0,256
Realizable 𝒌 − 𝝐 0,317 0,0419 0,256
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Open Water results
Periodic condition with cavitation model
Experimental comparatives
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Cavitation and Blockage results
Results Results with blockage correction
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Next steps
Analysis for lower cavitation number
Noted a high influence of blockage ratio in the cavitation area
Comparative between two blockage ratio for the same advance ratio of 0.249
Not contemplated in Glauert mode
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Research at superhydrophobic painting
Perform a numerical analysis of superhydrophobic surface on propeller
Trade-off between gain in performance and suction pressure
Boundary condition not
implemented
Using Field Functions and
storing previous results in
Monitors
Some results published in:
GOMES, G.G.; ESTEVES, F.R.; KATSUNO, E.T.; DANTAS, J.L.D. Simulations of Laminar–Turbulent Transition in foils using
CFD. 27º Congresso Internacional de Transporte Aquaviário, Construção Naval e Offshore. SOBENA. 2018.
Laminar-Turbulent transition
model
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Laminar to turbulent transition simulations using Gamma-
ReTheta turbulence model
Transition for the S9000 airfoil, α = 5.21 degrees.
Intermittency field (upper figure), alongside the wall shear stress for the upper
side of the airfoil, transition occurs between Rex = 9*10⁴ and 1.1*10⁵
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Bubble comparative
Comparison between the
separation bubble in the
upper side of the airfoil
obtained with the SST low-
Reynolds Turbulence model
(top) and with γ-Reθ (bottom)
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Turbulence Intensity
Use of ambient turbulent source to counteract turbulence decay
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Comparison with other turbulence models for simulations with low-Reynolds
number over airfoils
NACA43012A airfoil using different turbulence models with experimental data
Re = 6e4
Comparison with experimental values
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Conclusions
CFD has demonstrated great potential in assisting NAVAL-IPT experiments,
allowing new types of analysis and results to be incorporated into the laboratory
portfolio.
NAVAL-IPT will continue to improve its researchers to use this tool to offer more
specialized services to their clients
João Lucas Dozzi Dantas
Head of Laboratory
Naval Architecture and Ocean Engineering Laboratory
Center for Mechanical, Electrical and Naval Technologies