scholarly journals Numerical Study on the Tank Heel Determination Using Smoothed Particle Hydrodynamics

2021 ◽  
Vol 9 (9) ◽  
pp. 1016
Author(s):  
Kyu-Sik Park ◽  
Hung-Truyen Luong ◽  
Joonmo Choung
Keyword(s):  
Numerical Study ◽  
Center Of Mass ◽  
Fuel Tank ◽  
Suction Pump ◽  
Pump Operation ◽  
Fuel Tanks ◽  
Lng Fuel ◽  
Motion Characteristics ◽  
Lng Tank ◽  
Vessel Motion

Tank heel minimization is a significant issue in the design of LNG fuel tanks because it is associated with stable suction pump operation and thermal shock requirements during LNG bunkering. This study examined how the LNG tank heel is minimized, maintaining a suction pump fully submerged in LNG during dynamic vessel motion. The study assumed two LNG fuel tanks mounted on the forward deck of a 50,000 deadweight class oil product carrier. Information on the dimensions and shape of the LNG fuel tank was determined from Wartsila’s brochure, and the specifications of Vanzetti’s suction pump were referred to. The LNG fuel tank and LNG heel were modeled as rigid elements and hydrodynamically smoothed-particles, respectively. The number of particles could be determined by performing even keel analyzes by adding or subtracting particles until the target head was satisfied under the gravity load. To simulate the motion of the LNG fuel tank, the pitch and roll periods and amplitudes of the ship were calculated using the DNV classification rules. Visual observations of the dynamic flow during the pitch and roll motions with respect to the ship’s center of mass showed that the roll motion was more critical from the viewpoint of the LNG heel than the pitch motion. After performing the simulations for three cycles of roll and pitch motions, the suction pump submergence was reviewed in the last cycle. Under the conditions assumed in this study, a filling ratio of 15% was determined as the minimum LNG tank heel. Although the LNG heel has customarily been determined, the LNG heel needs to be determined through hydrodynamic analyses of each vessel because it depends on the shape of the fuel tank and the vessel motion characteristics.

Influence of welding residual stress on cryogenic materials applied to LNG fuel tanks for coastal vessels

2020 ◽  
Vol 34 (07n09) ◽  
pp. 2040031
Author(s):  
Tae-Yeob Kim ◽  
Je-Hyoung Cho ◽  
Sung-Won Yoon ◽  
Myung-Hyun Kim
Keyword(s):  
Residual Stress ◽  
Arc Welding ◽  
Local Buckling ◽  
Corrosion Damage ◽  
Fuel Tank ◽  
Welding Residual Stress ◽  
Fuel Tanks ◽  
Fundamental Research ◽  
Lng Fuel ◽  
Transient Thermal

The purpose of this paper is to investigate the influence of welding residual stress (WRS) of the liquefied natural gas (LNG) fuel tank. In general, WRS and distortions are caused by non-uniform temperature distribution by the welding heat source. This will not only cause a brittle fracture, local buckling and corrosion damage, but also adversely affect the fatigue strength of the welded structures. Since LNG is treated at cryogenic temperatures of −162[Formula: see text]C, leakage of LNG from the fuel tank to the outside may cause cracks in the hull and tank support system and cause severe damage. Therefore, it is necessary to predict the thermal behavior and WRS before welding is carried out. In this study, the WRS is calculated by thermal stress analysis based on the temperature distributions over time obtained from the transient thermal analysis. The results of this study can be used as a fundamental research for WRS analysis of plasma arc welding applied to LNG fuel tanks for coastal vessels.

Strength Assessment of Type ‘C’ LNG Fuel Tanks

2015 ◽  
Author(s):  
Bo Wang ◽  
Yung-Sup Shin ◽  
Eric Norris
Keyword(s):  
Failure Modes ◽  
Structural Integrity ◽  
Fuel Tank ◽  
Fe Model ◽  
Strength Evaluation ◽  
Integrity Assessment ◽  
Fuel Tanks ◽  
Complete Procedure ◽  
Type C ◽  
Lng Fuel

The objective of this study is to present a complete procedure for the strength evaluation of Type ‘C’ liquefied natural gas (LNG) fuel tanks. The fuel tank is designed independent of the ship’s hull and consists of double tanks with inside and outside supports. The inner tank, which holds the LNG cargo, is held within the outer tank using strap and cone supports at two ends. The outer tank is kept in vacuum and the space between the inner tank and the outer tank is filled with insulation materials. There are two saddle supports connecting the outer tank to the hull. The major components of the fuel tank in FE model include inner tank, outer tank, strap support, cone support, as well as two saddle supports. All these structures are designed to withstand all ship and service design loads. The inner tank is subjected to the internal pressure and the outer tank is loaded by external pressure. Due to the ship motion, the inertia forces caused by cargo accelerations will be applied to the tank structure. In this study, Finite Element (FE) analyses were performed in various load cases in which load components include design internal/external pressures, longitudinal / transverse / vertical accelerations, and gravity. Additionally, a Computational Fluid Dynamics (CFD) sloshing simulation on the fuel tank with splash baffles was performed to determine sloshing loads. Accidental load cases, including collision and flooding, were also considered in the structural analysis. Meanwhile, a buckling analysis on the evacuated outer tank was conducted to identify the critical collapse pressure. Acceptance criteria corresponding to yielding and buckling failure modes have been detailed for the strength evaluation of the Type ‘C’ LNG fuel tank. Thus, a complete procedure has been developed for the structural integrity assessment of tank and supporting structures for Type ‘C’ LNG fuel tanks.

Space Fitting Design of LNG Fuel Tank for a Small Truck and BOG Analysis of LNG Tank

2008 ◽  
Vol 32 (3) ◽  
pp. 379-386
Author(s):  
Alena Minkasheva ◽  
O-Woon Kwon ◽  
Sung-Joon Kim
Keyword(s):  
Fuel Tank ◽  
Lng Fuel ◽  
Lng Tank

Fuel Leaking Analysis of Fuel Tank by Projectiles Impact with Mechanical Properties of Projectiles

2013 ◽  
Vol 644 ◽  
pp. 203-206
Author(s):  
Hai Liang Cai ◽  
Bi Feng Song ◽  
Yang Pei ◽  
Shuai Shi
Keyword(s):  
High Speed ◽  
Drop Size ◽  
Fuel Tank ◽  
Size Distributions ◽  
Sauter Mean Diameter ◽  
Fuel Droplets ◽  
High Speed Impact ◽  
Fuel Tanks ◽  
Rigid Projectile ◽  
Drop Size Distributions

For making sure the dry bay ignition and fire, it’s necessary to calculate the number and the sizes of the droplets and determine the mass flow rate of the fuel induced by high-speed impact and penetration of a rigid projectile into fuel tank. An analytical model is founded and the method for calculating the initial leaking velocity of the fuel is determined. It gives the equation for calculating the drop size distributions of fuel and the Sauter mean diameter (SMD) of droplets, through the Maximum Entropy Theory and the conservation for mass. Using the Harmon’s equation for SMD,the fuel droplets SMD can be calculated. Results shows that the initial leaking velocity of the fuel is about linearly increasing with the velocity of the projectile, the SMD of fuel droplets increases with the hole size of the fuel tank which induced by the penetration of the projectile and linearly decreases with the velocity of the projectile. The results can be used for the ignition and fire analysis of the dry bay adjacent to fuel tanks.

Numerical Study of Viscous Flows Inside Partially Filled Spinning and Coning Cylinders

1996 ◽  
Vol 118 (2) ◽  
pp. 335-340 ◽  
Author(s):  
Mohamed Selmi
Keyword(s):  
Stokes Equations ◽  
Numerical Study ◽  
Center Of Mass ◽  
Steady Motion ◽  
Practical Interest ◽  
Nonlinear Effects ◽  
Navier Stokes ◽  
Navier Stokes Equations ◽  
Practical Applications ◽  
Analysis And Design

This paper is concerned with the solution of the 3-D-Navier-Stokes equations describing the steady motion of a viscous fluid inside a partially filled spinning and coning cylinder. The cylinder contains either a single fluid of volume less than that of the cylinder or a central rod and a single fluid of combined volume (volume of the rod plus volume of the fluid) equal to that of the cylinder. The cylinder rotates about its axis at the spin rate ω and rotates about an axis that passes through its center of mass at the coning rate Ω. In practical applications, as in the analysis and design of liquid-filled projectiles, the parameter ε = τ sin θ, where τ = Ω/ω and θ is the angle between spin axis and coning axis, is small. As a result, linearization of the Navier-Stokes equations with this parameter is possible. Here, the full and linearized Navier-Stokes equations are solved by a spectral collocation method to investigate the nonlinear effects on the moments caused by the motion of the fluid inside the cylinder. In this regard, it has been found that nonlinear effects are negligible for τ ≈ 0.1, which is of practical interest to the design of liquid-filled projectiles, and the solution of the linearized Navier-Stokes equations is adequate for such a case. However, as τ increases, nonlinear effects increase, and become significant as ε surpasses about 0.1. In such a case, the nonlinear problem must be solved. Complete details on how to solve such a problem is presented.

Updated Fuel Tank Puncture Survey: 1995-2020

2021 ◽  
Author(s):  
Karina Jacobsen
Keyword(s):  
Fuel Tank ◽  
Technical Data ◽  
Passenger Rail ◽  
Blunt Impact ◽  
Field Investigations ◽  
Fuel Tanks ◽  
Serious Injury ◽  
Conducting Research ◽  
Railroad System ◽  
General Operation

Abstract The Federal Railroad Administration’s Office of Research, Development and Technology has been conducting research into passenger fuel tank crashworthiness. The occurrence of a fuel tank puncture during passenger rail collisions and derailments increases the potential of serious injury and fatality for crew and passengers due to the possibility of fire. The purpose of the FRA research is to help support regulatory and standard development with technical data. In the last decade, the research has focused on understanding how fuel tanks are punctured during an impact and how various tank designs respond to common types of loading in collisions, derailments and general operation. Throughout the research, surveys have been conducted to determine the most likely scenarios that are causing fuel tank punctures. A previous FRA survey found that fuel tank punctures occur under two types of loading conditions: a blunt impact or a raking impact. A limited number of accident/incidents were evaluated in this survey. These incidents showed that fuel tanks are punctured on any side that is not protected or shielded. The purpose of this paper is to report on a recently conducted fuel tank puncture survey updated to include the last decade. This paper identifies and describes accidents and incidents that led to breached fuel tanks in freight and passenger trains traveling on the general railroad system in the U.S. between 2008 and 2020. The results include data from the FRA’s Railroad Accident/Incident Reporting System (RAIRS), queried from 1995 to 2020. This data include the number of recorded accidents/incidents and other trends like fuel spillage, operating authority and cause of accident/incident. RAIRS data showed accidents/incidents with fuel tank puncture ranging from 10 to 55 accidents/incidents per year. Additionally, more detailed results are shared from field investigations recently conducted by the FRA or Volpe Center. These more detailed investigations provide additional insight into the types of loading that may lead to a fuel tank puncture. This survey supplements the RAIRS data with more detailed information from field investigations. The paper finally discusses the conditions that lead to fire and the associated hazards.

An Investigation into the Motion Behaviour of a Wind Farm Mothership

2015 ◽  
Author(s):  
Blanca Peña ◽  
Erik P. ter Brake ◽  
Kyriakos Moschonas
Keyword(s):  
Numerical Simulations ◽  
Wind Farm ◽  
Wind Farms ◽  
Weather Conditions ◽  
Offshore Wind ◽  
Financial Benefit ◽  
Offshore Wind Farms ◽  
Motion Characteristics ◽  
Vessel Motion ◽  
Motion Behavior

A number of UK Round Three offshore wind farms are located relatively far from the coast making crew transfer to the sites time consuming, more prone to interruption by weather conditions and increasingly costly. In order to optimize the functionality of a permanent accommodation vessel, Houlder has developed a dedicated Accommodation and Maintenance Wind Farm vessel based on an oil & gas work-over vessel that has been successfully deployed for many years. The Accommodation and Maintenance (A&M) Wind Farm vessel is designed to provide an infield base for Marine Wind Farm operation. The A&M vessel is designed for high operability when it comes to crew access and performance of maintenance and repair of wind turbine components in its workshops. Also general comfort on board is of high regard. As such, the seakeeping behavior of the unit is of great importance. In this publication, the seakeeping behavior is presented on the basis of numerical simulations using 3D diffraction software. The first design iteration is driven by achieving high maneuverability and good motion characteristics for operational up-time and personnel comfort on board the vessel. Model test data of the original work-over vessel has been used to validate and calibrate the numerical simulations. On this basis, parametric studies can be performed to fine-tune a potential new hull form. In turn, this could reduce the number of required physical model tests providing a potential financial benefit and optimized delivery schedule. The vessel motion behavior was tested against the acceptability criteria and crew comfort guidelines of motion behavior for a North Sea environment.

scholarly journals Numerical Study of the Zero Velocity Surface and Transfer Trajectory of a Circular Restricted Five-Body Problem

2018 ◽  
Vol 2018 ◽  
pp. 1-10
Author(s):  
R. F. Wang ◽  
F. B. Gao
Keyword(s):  
Body Problem ◽  
Numerical Study ◽  
Dimensional Space ◽  
Center Of Mass ◽  
Three Dimensional ◽  
Regular Tetrahedron ◽  
Transfer Trajectory ◽  
Zero Velocity ◽  
Zero Velocity Surfaces ◽  
Zero Velocity Surface

We focus on a type of circular restricted five-body problem in which four primaries with equal masses form a regular tetrahedron configuration and circulate uniformly around the center of mass of the system. The fifth particle, which can be regarded as a small celestial body or probe, obeys the law of gravity determined by the four primaries. The geometric configuration of zero-velocity surfaces of the fifth particle in the three-dimensional space is numerically simulated and addressed. Furthermore, a transfer trajectory of the fifth particle skimming over four primaries then is designed.

Study Regarding the Influence of the Fuel Tank Constructive Characteristics on Slosh-Noise Effect

2016 ◽  
Vol 834 ◽  
pp. 22-27 ◽  
Author(s):  
Oana Maria Manta Balas ◽  
Radu Balas ◽  
Cristian Vasile Doicin
Keyword(s):  
The Body ◽  
Fuel Tank ◽  
Noise Effect ◽  
Great Achievement ◽  
Fuel Tanks ◽  
Entire Vehicle ◽  
Body In White ◽  
Innovative Potential ◽  
The Impact ◽  
The Waves

The aim of this article is to highlight the impact of the fuel movements inside the plastic fuel tank (waves) for the client perception of noise. Today there isn’t a clear methodology regarding the reproducing the fuel waves, but there are different approaches to be taken into account and also there is an innovative potential. Due to the fast technological progress the body in white and not only, the entire vehicle became lighter and lighted. A consequence of this great achievement is that the client can hear easier the sound produced by different components of the car. The plastic fuel tank can be considered such a component. The authors have done a deep analysis of present automotive fuel tanks and propose solutions for breaking the waves produced inside fuel tanks, so as to reduce the slosh noise effect. The studies will be continued during the doctoral approach of the first author.

scholarly journals Experimental and Numerical Study on Hydrodynamic Performance of an Underwater Glider

2018 ◽  
Vol 2018 ◽  
pp. 1-13
Author(s):  
Yanji Liu ◽  
Jie Ma ◽  
Ning Ma ◽  
Zhijian Huang
Keyword(s):  
Reynolds Number ◽  
Degrees Of Freedom ◽  
Numerical Study ◽  
Similarity Theory ◽  
Dynamics Simulation ◽  
Hydrodynamic Performance ◽  
Hull Design ◽  
Motion Characteristics ◽  
6 Degrees Of Freedom ◽  
Temperature Depth

The hydrodynamic coefficients are important parameters for predicting the motion of the glider and upgrading the hull design. In this paper, based on the Reynolds number similarity theory, 6 degrees of freedom (DOFs) of the fluid force and torque of a 1:1 full-scale glider model are measured. The present measurements were carried out at (2 - 14m/s) by varying attack angles and sideslip angles (-9 - 9°), respectively. The measurements were used to study the variation of the hydrodynamics of the glider, and the measurements have also been used to validate results obtained from a CFD code that uses RNG k-ε. The hydrodynamic force coefficients obtained from CFD accord well with the measurements. However, the torque coefficients difference is fairly large. Dynamics simulation results show that CFD results can be used to design and study the motion characteristics of gliders. In order to simplify the design process of gliders, we fit the empirical formula based on the experimental data and obtain a drag coefficient equation with Reynolds number. The influence of two kinds of appendages of the Conductance-Temperature-Depth (CTD) unit and thruster unit on the glider drag were studied by a contrast test. The analysis results can provide reference for design and the motion investigate of gliders.

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