DEVELOPMENTS of HYDRODYNAMICS MODELING

International Marine & OffShore
Engineering Conference
DEVELOPMENTS of HYDRODYNAMICS MODELING TECHNIQUES for
UNDERWATER VEHICLES
SERTAC ARSLAN,
Asst. Prof. HAYRI ACAR
and Prof. MEHMET SERIF
KAVSAOGLU
International Marine & Offshore Engineering Conference 2014
CONTENTS
 INTRODUCTION & MOTIVATION
 DEFINITION OF THE HYDRODYNAMIC COEFFICIENTS
 METHODOLOGY OF THE CFD ANALYSIS PROCESS
 VERIFICATION OF HYDRODYNAMIC ANALYSIS MODEL
 HYDRODYNAMIC ANALYSIS of AUTOSUB UNDERWATER VEHICLE
 CONCLUSION
International Marine & Offshore Engineering Conference 2014
MOTIVATION
 In this project, new hydrodynamic modeling techniques
are developed and all hydrodynamic coefficients of an
AUV are calculated in six degree of freedom (6 DOF), by
using the developed calculation methods.
 Firstly, a new hydrodynamic calculation model for
underwater vehicles is created and verified.
 After the verification of CFD solution model,
hydrodynamic database of an AUV is constituted and
then static stability characteristics are determined.
International Marine & Offshore Engineering Conference 2014
INTRODUCTION
In recent years, AUVs have become a
main tool for surveying below the sea
in the scientific, military and
commercial applications because of
the significant improvement in their
performance.
In order to design an AUV, it is usually necessary to analyze its hydrodynamics performance,
maneuverability and controllability characteristic.
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INTRODUCTION
To be examined AUV's performance in the simulation environment; hydrodynamic equations of
motion should be established, then hydrodynamic force and moments values should be fed to the
equations of motion ​, and simulation studies should be performed in required maneuvering
scenarios.
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INTRODUCTION
The hydrodynamic coefficients may be classified into 2 main groups.
 Static hydrodynamic coefficients
 Dynamic hydrodynamic coefficients
Also, dynamic coefficients may be classified into 3 subgroups such as;
 Linear damping coefficients (maneuvering coefficients),
 Linear inertial force coefficients (added mass, inertia coefficients)
 Nonlinear damping coefficients
These coefficients can be obtained by different ways. These are experimental methods,
numerical methods (CFD) and empirical methods.
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INTRODUCTION
Rotating-Arm Mechanism
Planar Motion Mechanism
Vertical Planar Motion and Rotating-Arm Mechanism are the most common experimental techniques
to measure the hydrodynamic coefficients. Static coefficients, maneuvering coefficients and added
mass-inertia coefficients can be calculated in these mechanisms.
Using experimental techniques to calculate the hydrodynamic coefficients is a very expensive method.
Instead of experimental methods, numerical (computational fluid dynamics) and empirical techniques
can be developed and used.
International Marine & Offshore Engineering Conference 2014
DEFINITION OF THE HYDRODYNAMIC COEFFICIENTS
The coefficients, which mostly affect the maneuverability of an AUV, are static and
the linear damping (maneuvering) coefficients.
A rectangular Cartesian coordinate system attached to the vehicle.
The three components of
the hydrodynamic force
along the directions x, y, z
are denoted by X, Y, Z
respectively, and the three
components of the
hydrodynamic moments
by L, M, N.
International Marine & Offshore Engineering Conference 2014
DEFINITION OF THE HYDRODYNAMIC COEFFICIENTS
The three components of force X, Y, Z and the three components of the moments L, M, N are
expanded up to second order terms in the linear and angular velocities u, v, w, p, q, r and the
coupled of them.
And added mass coefficients should also be taken into consideration.
International Marine & Offshore Engineering Conference 2014
DEFINITION OF THE HYDRODYNAMIC COEFFICIENTS
Added mass can be modeled as some volume of fluid moving with the object. So, added mass
coefficients must be considered and added to the equation of motions. For underwater
vehicles added-mass coefficients are constant and independent of maneuvering and wave
effects.
In the added mass matrix the diagonal terms are always positive, and those terms are dominant to
dynamics of vehicle. If the vehicle is symmetrical, the terms except diagonal terms can be
neglected.
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METHODOLOGY OF THE CFD ANALYSIS PROCESS
In this study, time-independent hydrodynamic coefficients of an AUV will be calculated and hydrodynamic
database of the AUV will be created. Previous of the calculation of hydrodynamic coefficients of AUV,
hydrodynamic modeling method will be created and verified by a benchmark study.
In this study, 3D solid modeling
program CATIA, ANSYS GAMBIT and
TGRID meshing programs and
ANSYS FLUENT commercial program
is used.
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VERIFICATION OF HYDRODYNAMIC ANALYSIS MODEL
In order to calculate hydrodynamic coefficients correctly by using CFD methods, Benchmark
study has to be done.
In order to evaluate the capabilities and accuracy of the tools used in this project, DARPA
SUBOFF model has been selected as test case.
DARPA model was designed at
David Taylor Research Center in
order to provide a forum for the
CFD community to compare the
numerical computations of the
flow field over an axisymmetric
hull model with and without sail
Length: 4 m
and appendages.
Diameter: 0,508 m
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TEST AND ANALYSIS CONDITIONS
The data used in the present study are based on the experiments which were performed in the David
Taylor Model Basin on Towing Carriage by David Taylor Research Center . Three configurations of
DARPA SUBOFF model are studied and compared with available test results in this report.
 Bare hull
 Hull with sail
 Hull with sail and appendages
The static stability experiments were conducted at zero angle of attack and a model speed of 9m/s
which correspond to a Reynolds number of about 30 million. In the calculation of Reynolds Number,
kinematic viscosity of the water is accepted as 1,307e-06 m2/s.
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INVESTIGATIN OF TEST CASE MODELS
1.Bare Hull Model
Bare hull configuration of DARPA model consists of nose, body and aft-body parts.
2. Hull with Sail Model
Hull with sail configuration of DARPA model consists of nose, body, aft-body, and sail parts.
3. Hull with Sail and Appendages Model
Hull with sail configuration of DARPA model consists of nose, body, aft-body, sail and four appendages
parts.
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GRID GENERATION
3D grid generation is used for the all
configurations. In order to constitute the
grid of the AUV GAMBIT 2.4 software is
used. Grids are created in high quality to
use in Navier-Stokes equations.
To define the boundary layer over the
Autosub geometry TGRID 5.0 software is
used. The boundary layer is created as two
zones. These are inner zone and outer zone.
Y+ value is chosen 1 for this study.
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GRID GENERATION
At the end of grid generation process, vehicle’s grid and fluid domain’s grid is completed, and
the geometry get ready to make hydrodynamic analyses in CFD software.
In this study, Navier-Stokes equations are solved
with following conditions,
 Segregated solver model,
 K-ε Realizable turbulence model,
 Y+ ~ 1 is chosen.
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RESULTS AND VERIFICATION OF CFD ANALYSES
Three different configurations of DARPA model is analyzed in this study. Analyses are done in
9m/s speed and 20 m depth.
Analysis Results of Bare Hull Model
Experimental results of pressure and friction coefficients
are compared with CFD analysis results.
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RESULTS ANS VERIFICATION OF CFD ANALYSES
Analysis Results of Hull with Sail Model
Experimental results of pressure coefficients and friction coefficients over the hull and sail are
compared with CFD results for this configuration.
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RESULTS ANS VERIFICATION OF CFD ANALYSES
Analysis Results of Hull with Sail and Appendages Model
Pressure coefficients measurement results exist for this configuration, in three stations on the
appendages. These stations which presents on the appendages, are located in distance of 10%, 50% and
90% of the total appendages length, respectively. Comparison of pressure coefficients results of
appendages stations which is calculated in CFD analyses with experimental results. 25% of the chord is
accepted as zero point in the graphics.
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RESULTS ANS VERIFICATION OF CFD ANALYSES
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HYDRODYNAMIC ANALYSIS of AUTOSUB
AUTONOMOUS UNDERWATER VEHICLE (AUV)
Autosub is a large AUV developed by a team of
engineers and oceanographers at the National
Oceanography Centre, Southampton, UK.
Autosub has been employed in scientific research
projects ranging from mapping manganese’s
distributions in a sea.
Autosub is controlled by four movable control
surface mounted at the rear of the vessel in a
cruciform arrangement. The control surfaces’ cross
sections consist of NACA 0015 hydrofoil.
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ANALYSIS CONDITIONS
In this study, a comprehensive study has been made to constitute hydrodynamic database of
Autosub AUV in six degree of freedom (6DOF).
X, Y, Z forces and K, M, N moments of Autosub is calculated for different maneuvering
conditions.
 Velocity levels: 5, 10, 15, 20 and 25 knots.
 Angle of attacks: 10, -7, -5, -2, 0, 2, 5, 7, and 10
 Sideslip angels: 10, -7, -5, -2, 0, 2, 5, 7, and 10
 Elevator deflections: 0, ±5, ±10, ±15, ±20 degrees
 Rudder deflections: 0, ±5, ±10, ±15, ±20 degrees
 Turn Radius: 20, 30, 40
 Operating Reynolds Number is between: 1,27e+07 - 6,52e+07.
 Kinematic viscosity of the water is accepted as 1,38e-06.
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GRID GENERATION OF AUTOSUB
3D grid generations are used for all analyses. In
order to constitute the grid of the Autosub, GAMBIT
2.4 software is used.
Quite quality mesh is used for suitable solution with
Navier-Stokes Equations.
In order to obtain significant result and to be time
efficient node numbers in the grids are optimized.
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ANALYSIS RESULTS OF AUTOSUB
In this study, hydrodynamic database of Autosub AUV is constituted in 6DOF by using verified
CFD calculation model for underwater vehicles.
Around the critical Reynolds number, the stability
characteristic of fluids is unstable. It is shown that,
the flow regime where Autosub cruise in is far away
from the critical Reynolds number and stable.
Increment of drag force is compatible with velocities
Variation of the axial forces with angle of attacks is
too much in high speeds and very little in low speeds.
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ANALYSIS RESULTS OF AUTOSUB
 Yaw force decrease with sideslip angle
according to velocity levels.
 Variation of pitching moment is
investigated in 10 knots cruise condition.
 Pitching moment increase with angle of
attack for different elevator deflections.
 Trim conditions of Autosub in pitch plane
can also be checked.
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ANALYSIS RESULTS OF AUTOSUB
Longitudinal static stability can be investigated according to
CM-α graphics.
𝑆𝑡𝑎𝑡𝑖𝑐 𝑆𝑡𝑎𝑏𝑖𝑙𝑖𝑡𝑦 𝐶𝑟𝑖𝑡𝑒𝑟𝑖𝑎 =>
𝜕𝐶𝑀
<0
𝜕𝛼
Autosub has statically unstable geometry.
 This is because of the center of gravity point is the behind of
center of pressure point of Autosub. Center of gravity point
distance to the nose of the geometry is 3.159 meter but, the
resultant hydrodynamic force point is in front of the center of
gravity.
 In the Autosub geometry, aft-body part produces a
negative lift; in this situation the center of the pitch
moment moves to front of the vehicle and this situation
pushes forwards the center of pressure point in front of
the center of the gravity point, so that the geometry
becomes unstable.
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CONCLUSION
 In the scope of this study, dynamic stability analyses and performance analyses of Autosub
are also performed.
 After the stability analyses, it can be said that, these underwater geometries such as
Autosub are usually statically unstable but dynamically stable. Because of the specific
damping effects of underwater worlds such as cross coupled terms, added mass terms and
munk moments, underwater vehicles stability characteristics get stable.
 In the hydrodynamic analyses, it can be said that; Reynolds Averaged Navier Stokes (RANS)
equations are solved without any problem and the verified CFD calculation models can be
used to calculate any of hydrodynamic coefficients in 6 degree of freedom.
 In this project; a new numerical and empirical hydrodynamic calculation method is
developed to calculate hydrodynamics coefficients of Autosub AUV in 6DOF.
 Calculated numerical results are compared with the experimental results and it is seen that,
calculated results are close to experimental results adequately, to rely on performing
hydrodynamic analyses with CFD methods.
 In this project, a new hydrodynamic analysis method is developed and verified for
underwater vehicles. By using the verified analysis models, hydrodynamic performance and
characteristic of any underwater vehicles can be investigated and determined.
International Marine & Offshore Engineering Conference 2014
REFERENCES
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Aerospace Engineering, Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and
State University.
(2) Data Sheet, Overview of Model Testing Facilities, NTNU.
(3) Fossen, T., I., 1994: “Guidance and Control of Ocean Vehicles, Wiley, H., Sons, 5-90.
(4) Gertler, M., Grant, R. H., 1967: Standard Equations of Motion for Submarine Simulations.
(5) Huang, T., Liu, H-L, Groves, N., Forlini, T., Blanton, J., Growing, S., 1994: Measurement of Flows over an
Axisymmetric Body with Various appendages in a Wind Tunnel: the DARPA Suboff Experimental Program,
David Taylor Model Basin, Washington, USA.
(6) Jones, D. A., Clarke, D. B., Brayshaw, I. B., Barillon, J. L, and Anderson B., 2002: The Calculation of
Hydrodynamic Coefficients for Underwater Vehicles, Maritime Platforms Division/Platform Sciences
Laboratory, Australia.
(7) Jun, B. H., Park, J. Y., Lee, F. Y., Lee, P. M., Lee, C. M., Kim, K., Lim, Y. Y. and Oh, J. H. (2009). Development
of the AUV ISIMI and a free running test in an Ocean Engineering Basin, Ocean Engineering Research
Department, Republic of Korea.
(8) Nancy, C. G., Thomas, T. H., Ming, S. C,. 1989: Geometric Characteristic of Darpa Suboff Model, Ship
Hydromechanics Department, David Taylor Research Center, USA.
(9) Phillips, A., Furlong, M., Turnock, S. R., The Use of Computational Fluid Dynamics to Determine the Dynamic
Stability of an Autonomous Underwater Vehicle, National Oceanography Center, Southampton, England.
(10) http://www.km.kongsberg.com
(11) http://www.noc.soton.ac.uk
(12) http://web.mit.edu/towtank/www/
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THANKS…
ANY QUESTIONS?
International Marine & Offshore Engineering Conference 2014