To see the other types of publications on this topic, follow the link: Marine propeller.

Dissertations / Theses on the topic 'Marine propeller'

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the top 50 dissertations / theses for your research on the topic 'Marine propeller.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Browse dissertations / theses on a wide variety of disciplines and organise your bibliography correctly.

1

Chang, Bong Jun. "Application of CFD to marine propellers and propeller-hull interactions." Thesis, Imperial College London, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.286067.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Mosaad, Mohamed Ahmed Abdel-Rahman. "Marine propeller roughness penalties." Thesis, University of Newcastle Upon Tyne, 1986. http://hdl.handle.net/10443/1006.

Full text
Abstract:
The main objective of the project is to investigate the influence of surface roughness of marine propeller blades on propulsive power. The work has involved studies in the concept and practice of surface roughness measurement and characterisation as well as application of boundary layer theory for the analysis propeller-ship hull flow interaction of propeller flow and propellar-ship hull flow interaction. From extensive measurements of the surface topography of in-service propellers, a standard measurement procedure using different commercially available propeller-surveying instruments is described. A development of turbulent boundary layer procedures has been made to determine sufficiently accurately the increment of drag coefficient of propeller blade sections due to propeller blade surface roughness. The roughness function used for this integral boundary layer analysis is derived using, principally, Musker's experimental data. In addition, an experimental determination of the roughness function of a replicated propeller surface using a rotor apparatus has been carried out and described in detail. The turbulent boundary layer procedures require a knowledge of the surface variation of pressure over the propeller blade. For this purpose a program based on Riegels method has been used to give the velocity distribution for a given propeller section geometry. This is used with the boundary layer procedures for developing a complete program "PROFNESS" to calculate the increment of drag coefficient of the blade section. Results from different propellers analysed indicate that the power penalty is proportional to the relative blade roughness to the 1/3 power. An investigation has been made to compare the increment of frictional coefficient for a flat plate and propeller section profiles. It is shown that a "rough" flat plane calculation is quite adequate for such work.' The use of a flat plate analogue as a reference to calculate the skin friction resistance of both propeller and hull surfaces is considered. It is shown that the proposed solution of flat plate momentum integral equations provides a valid, simple and practical solution to the problem of predicting the hull and propeller roughness drag penalties. It also provides, particularly for ship hull resistance, a strong support for the ITTC Correlation Line, not only, and importantly, in regard to its slope, but also its level. For shipowners and operators who may not wish to access advanced computer programs, a simplified method has been proposed to calculate the propeller roughness penalties. There is a good agreement between the two simplified and detailed propeller analysis methods. The propeller roughness penalties, which can be obtained from either the simplified or the more rigorous method, can be related to the Rubert Propeller Comparator Gauges in order to quantify the benefits and justify the cost of the blade surface roughness. Analytical procedures have been included which can be used to calculate the combined effects on ship performance of propeller blade and ship hull surface roughnesses.
APA, Harvard, Vancouver, ISO, and other styles
3

Le, Guen-Geffroy Antoine. "Marine ageing and fatigue of carbon/epoxy composite propeller blades." Thesis, Brest, 2019. http://www.theses.fr/2019BRES0104.

Full text
Abstract:
Les travaux présentés portent sur l’étude du vieillissement en milieu marin d’un composite carbone époxy pour applications pâles d’hélice de navires. La caractérisation de la prise en eau dans la résine pure et le composite a montré un comportement Fickien. La présence d’eau dans les porosités du composite a également été mise en évidence analytiquement. Le vieillissement accéléré de la résine a mis en évidence trois phénomènes : l’oxydation, le vieillissement physique et la plastification. L’effet mécanique de ces deux derniers a été particulièrement étudié. La présence d’eau et donc d’une résine plastifiée a eu l’effet d’accélérer le vieillissement physique. L’effet du vieillissement accéléré sur le composite a ensuite été étudié sous différentes sollicitations quasi statiques et de fatigue. Peu d’effets de l’eau ont été relevés pour les sollicitations de traction sur des orientations sens fibres. Cependant, des pertes de plus importantes des propriétés mécaniques ont été observés en traction sens transverse aussi bien en statique qu’en fatigue. Ces mêmes résultats ont été trouvés sous sollicitations de flexion grâce à l’essai de flexion quatre points. Ce dernier a été discuté du fait de l’endommagement qu’il provoque. Enfin, le composite a été étudié sous sollicitations de délaminage suivant deux modes de fissuration: ouverture et cisaillement dans le plan. La présence d’eau a eu pour effet de diminuer l’énergie de fissuration dans les deux modes. Ce même résultat a été trouvé sous chargement de fatigue. L’influence du vieillissement physique sur les propriétés mécaniques du composite a également été démontré, son effet étant négatif, il nécessite d’être pris en compte
The current document presents the long term seawater ageing effect on the fatigue properties of carbon fibre reinforced epoxy marine propeller blades. Seawater uptake in the resin and the composite was identified to correspond to a Fickian diffusion. Calculations of the mass to saturation of the composite based on that of the resin reveal the presence of water in the composite’s porosities.Accelerated ageing of the pure resin highlighted three ageing phenomena: oxidation, plasticization and physical ageing. The last two were mechanically characterized separately and coupled with one another. Above all, it was shown that the presence of seawater accelerated the physical ageing kinetics by reducing the relaxation time. The composite was studied under different quasistatic and cyclic loadings.Few effects of seawater have been found for tensile stresses on fibre oriented loadings. This was not the case for transversely loaded composite that showed a non-negligible decrease of the mechanical properties for both static and fatigue loadings. This was also the case for flexure loading which was studied under four-point flexure. This latter test method was particularly studied due to the particular induced damage. The composite was studied under two delamination loadings: crack opening and inplane shear. It was observed that seawater decreased the critical strain energy release rates for both load cases as well of the fatigue resistance of both crack modes. Finally, the effect of physical ageing on the composite was studied and found to be non-negligible, demonstrating the necessity of taking it into account for both ageing and mechanical design
APA, Harvard, Vancouver, ISO, and other styles
4

Matusiak, Jerzy. "Pressure and noise induced by a cavitating marine screw propeller." Espoo : Valtion teknillinen tutkimuskeskus, 1992. http://catalog.hathitrust.org/api/volumes/oclc/25913793.html.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Ahl, Daniel. "Analysis of how different mesh functions influence the result in CFD-simulation of a marine propeller :." Thesis, Karlstads universitet, Avdelningen för energi-, miljö- och byggteknik, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:kau:diva-28644.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Taylor, Todd Eric. "Combined experimental and theoretical determination of effective wake for a marine propeller." Thesis, Massachusetts Institute of Technology, 1994. http://hdl.handle.net/1721.1/12299.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Dagres, Ioannis. "Simulation-guided lattice geometry optimization of a lightweight metal marine propeller for additive manufacturing." Thesis, Massachusetts Institute of Technology, 2019. https://hdl.handle.net/1721.1/122309.

Full text
Abstract:
Thesis: Nav. E., Massachusetts Institute of Technology, Department of Mechanical Engineering, 2019
Thesis: S.M., Massachusetts Institute of Technology, Department of Mechanical Engineering, 2019
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 149-153).
Additive manufacturing (AM) is one of the most promising emerging technologies for advanced mechanical systems. When compared to conventional manufacturing processes, AM offers major advantages in production of complex components, enhanced performance, material savings, and supply chain management. These advantages are driving a shift towards AM in marine industry, which is highlighted by recent relative publications of the American Bureau of Shipping (ABS) and others. This thesis focuses on the design of an exemplary marine propeller that leverages the advantages of AM through simulation-guided design of an internal lattice structure. Specifically, a B-series Wageningen three-blade propeller model, provided by Naval Warfare Surface Center (NSWC) Carderock, was used as a baseline. Its open water loading conditions were calculated numerically using OpenFOAM®, a computational fluid dynamics (CFD) software. The CFD results were verified using the provided test data, the thrust and torque coefficients differed by a maximum of 2.7%. The derived loads were introduced to the Finite Element Analysis (FEA) based optimization utility in Autodesk® Netfabb Ultimate, in order to identify the optimum lattice geometry for this application. The design limitations were dictated by the material (316SL stainless steel), the metal additive manufacturing process, and the propeller outer geometry.A variety of lattice infill designs were generated to create a design trade space and conclude to the most appropriate design for this application. The design with the best performance was a hexagonal grid lattice with 1 mm wall thickness, which was prescribed as a manufacturing constraint (i.e., the thinnest wall). The material volume was reduced by more than 50%, while exhibiting a satisfactory safety factor based on the material properties and the simulated loads. Sections of the propeller were prototyped by Desktop Metal Studio System[superscript TM].
by Ioannis Dagres.
Nav. E.
S.M.
Nav.E. Massachusetts Institute of Technology, Department of Mechanical Engineering
S.M. Massachusetts Institute of Technology, Department of Mechanical Engineering
APA, Harvard, Vancouver, ISO, and other styles
8

Turnock, Stephen Richard. "Prediction of ship rudder-propeller interaction using parallel computations and wind tunnel measurements." Thesis, University of Southampton, 1993. https://eprints.soton.ac.uk/48365/.

Full text
Abstract:
A theoretical method has been developed to predict the forces developed due to the interaction between a ship rudder and propeller. A parallel lifting suface panel program (PALISUPAN) ha sbeen written in Occam2 which is designed to run across variable sized square arrays of transputers. thsi program forms teh basis of the theoretical method. The rudder and propeller are modelled separately. Their interaction is accounted for through an iterative process whereby their respective inflow velocity fields are modified using a circumferential average of the disturbance velcoity due to the other body. Prior to writing PALISUPAN, software techniques for the implementation of computational fluid dynamics algorithms across arrays of transputers were developed. The approach used is based on a geometric parallelism. At the outermost level on each transputer the particular CFD algorithm runs in parallel with a harness process. The harness controls teh communication across teh transputer array. to prove thsi concept an explicit finite volume solver for the two-dimensional Euler equations has been implemented. PALISUPAN itself uses a perturbation potential formulation and an explicit zero pressure loading condition is enforced at the trailing edge. Use of the communications harness greatky reduces code development time and although an implicit solver PALISUPAN gives good parallel performance. Wind tunnel tests were undertaken to derive experimental data for validation of the prediction method. These used a 3.5m x 2.5m low speed widn tunnel and a range of flow an dgeometrical parameters were tested. Total rudder forces and moments, propeller thrust and torque and quasi-steady rudder surface pressures were measured. Empirical relationships for teh prediction of rudder lift, drag and stall for use in ship manoeuvring studeis were also derived. The validated theoretical prediction for rudder-propeller interaction using PALISUPAN allows the detailed design of sjip rudder-propeller systems to be enhanced. The parallel performance of the pALISUPAN demonstrates the practicality of using transputer arrays to solve CFD problems.
APA, Harvard, Vancouver, ISO, and other styles
9

Stewart, David Paul James. "Characteristics of a ship's screw wash and the influence of quay wall proximity." Thesis, Queen's University Belfast, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.296798.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Eastridge, Jonathan R. "Investigation and Implementation of a Lifting Line Theory to Predict Propeller Performance." ScholarWorks@UNO, 2016. http://scholarworks.uno.edu/honors_theses/72.

Full text
Abstract:
Numerous hydrodynamic theories may be used to predict the performance of marine propellers. The goal of this thesis is to investigate and implement a lifting line theory as a program written in FORTRAN and to test its capabilities on some Wageningen B-Series propellers. Special attention is given to the validation of the routines involved in the implementation of the theory. Difficulties were experienced in obtaining results that accurately reflect the published experimental results, and some discussion is included regarding possibilities for the sources of these errors. Also discussed are the results of other lifting line codes and their respective differences from the current implementation.
APA, Harvard, Vancouver, ISO, and other styles
11

Wang, Dazheng. "The development and validation of propeller design methods incorporating new approaches to blade section design." Thesis, University of Newcastle Upon Tyne, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.261266.

Full text
APA, Harvard, Vancouver, ISO, and other styles
12

Gaschler, Maria [Verfasser], and Moustafa [Akademischer Betreuer] Abdel-Maksoud. "Numerical modelling and simulation of cavitating marine propeller flows / Maria Gaschler ; Betreuer: Moustafa Abdel-Maksoud." Hamburg : Universitätsbibliothek der Technischen Universität Hamburg-Harburg, 2017. http://d-nb.info/1136955143/34.

Full text
APA, Harvard, Vancouver, ISO, and other styles
13

Zisman, Zachary Samuel. "On the Simulation of an All Electric Ship Powertrain Utilizing a Surface Piercing Propeller Via a Modular Main Propulsion Plant Model." Thesis, Virginia Tech, 2011. http://hdl.handle.net/10919/33241.

Full text
Abstract:
A modular simulation model of a marine powertrain consisting of a prime mover, propeller shaft, propulsor, and control system was developed, tested, and used to demonstrate the ability to analyze the marine powertrain numerically. The modularity of the model allows for the user to easily substitute different or more advanced modules, or add additional modules to obtain a greater level of detail or simulate more complex interactions of systems with the marine powertrain. Current and historical trends indicate an interest in all electric ship design, and the use of surface piercing propellers for small craft. Due to the availability of towing tank data from a surface piercing propeller, an all electric prime mover module, surface piercing propeller module, propeller shaft module, and PID control module were coded, integrated, and operated, simulating a complete powertrain. Simulations were conducted using full-scale real-world conditions to demonstrate the model functionality and level of detail. Simulation results provided insight into the vibrational excitation, stability, and control of such a powertrain.
Master of Science
APA, Harvard, Vancouver, ISO, and other styles
14

Jennings, Stephen Gregory. "Creation, Verification, and Validation of a Panel Code for the Analysis of Ship Propellers in a Steady, Uniform Wake." ScholarWorks@UNO, 2010. http://scholarworks.uno.edu/td/1209.

Full text
Abstract:
This report describes the governing equation and boundary conditions for a marine propeller operating in a uniform flow field of inviscid and irrotational fluid. A method is presented by which the velocity and pressure on the blade surface of the propeller can be numerically simulated, using hyperboloidal, constant strength source and doublet panels. Accuracy of the numerical method is verified through comparison with analytically known results and the ability of the numerical simulation to predict the thrust and torque on a propeller in open water is assessed through comparison with published experimental results. The thrust and torque results for the propeller are near the experimental measurements but do not converge to a common value as the panel size decreases.
APA, Harvard, Vancouver, ISO, and other styles
15

Radan, Damir. "Integrated Control of Marine Electrical Power Systems." Doctoral thesis, Norwegian University of Science and Technology, Faculty of Engineering Science and Technology, 2008. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-1984.

Full text
Abstract:

This doctoral thesis presents new ideas and research results on control of marine electric power system.

The main motivation for this work is the development of a control system, power management system (PMS) capable to improve the system robustness to blackout, handle major power system faults, minimize the operational cost and keep the power system machinery components under minimal stress in all operational conditions.

Today, the electric marine power system tends to have more system functionality implemented in integrated automation systems. The present state of the art type of tools and methods for analyzing marine power systems do only to a limited extent utilize the increased knowledge available within each of the mechanical and electrical engineering disciplines.

As the propulsion system is typically consisted of the largest consumers on the vessel, important interactions exists between the PMS and vessel propulsion system. These are interacted through the dynamic positioning (DP) controller, thrust allocation algorithm, local thruster controllers, generators' local frequency and voltage controllers. The PMS interacts with the propulsion system through the following main functions: available power static load control, load rate limiting control and blackout prevention control (i.e. fast load reduction). These functions serve to prevent the blackout and to ensure that the vessel will always have enough power.

The PMS interacts with other control systems in order to prevent a blackout and to minimize operational costs. The possibilities to maximize the performance of the vessel, increase the robustness to faults and decrease a component wear-out rate are mainly addressed locally for the individual control systems. The solutions are mainly implicative (for e.g. local thruster control, or DP thrust allocation), and attention has not been given on the interaction between these systems, the power system and PMS. Some of the questions that may arise regarding the system interactions, are as follows: how the PMS functionality may affect a local thruster control, how the local thruster control may affect the power system performance, how some consumers may affect the power system performance in normal operations and thus affect other consumers, how the power system operation may affect the susceptibility to faults and blackout, how various operating and weather conditions may affect the power system performance and thus propulsion performance though the PMS power limiting control, how propulsion performance may affect the overall vessel performance, which kind of faults can be avoided if the control system is re-structured, how to minimize the operational costs and to deal with the conflicting goals. This PhD thesis aims to provide answers to such questions.

The main contributions of this PhD thesis are:

− A new observer-based fast load reduction system for the blackout prevention control has been proposed. When compared to the existing fast load reduction systems, the proposed controller gives much faster blackout detection rate, high reliability in the detection and faster and more precise load reduction (within 150 miliseconds).

− New advanced energy management control strategies for reductions in the operational costs and improved fuel economy of the vessel.

− Load limiting controllers for the reduction of thruster wear-out rate. These controllers are based on the probability of torque loss, real-time torque loss and the thruster shaft

accelerations. The controllers provide means of redistributing thrust from load fluctuating thrusters to less load fluctuating ones, and may operate independently of the thrust allocation system. Another solution is also proposed where the load limiting controller based on thrust losses is an integrated part of DP thrust allocation algorithm.

− A new concept of totally integrated thrust allocation system, local thruster control and power system. These systems are integrated through PMS functionality which is contained within each thruster PLC, thereby distributed among individual controllers, and independent of the communications and dedicated controllers.

− Observer-based inertial controller and direct torque-loss controller (soft anti-spin controller) with particular attention to the control of machine wear-out rate. These controller contribute to general shaft speed control of electrical thrusters, generators and main propulsion prime movers.

The proposed controllers, estimators and concepts are demonstrated through time-domain simulations performed in MATLAB/SIMULINK. The selected data are typical for the required applications and may differ slightly for the presented cases.

APA, Harvard, Vancouver, ISO, and other styles
16

Jing, Zhenrong. "Simulations Numériques des Transitions de Couche Limite sur des Pales en Rotation : Eolienne à Axe Horizontal et Hélice Marine." Thesis, Ecole centrale de Nantes, 2020. http://www.theses.fr/2020ECDN0035.

Full text
Abstract:
Les couches limites des Eolienne à Axe Horizontal (HAWT) et des hélices marines partagent un point commun avec l'écoulement de von Kármán, qui est créé par un disque rotatif immensé dans un fluide. L'écoulement de von Kármán peut induire une transition par écoulement transverse aussi dite "corss-flow". L'objet de la présente étude est la possibilité d'une transition d'écoulement transversal sur les HAWT et les hélices marines. Cette étude montre que les transitions naturelle de couche limite sur les HAWTs et les hélices marine sont induites par des mécanismes distinctement différents. Le résultat de l'écoulement autour d'un pale de HAWT montre que le profil de la couche limite est très proche d'un profil bidimensionnel. Sur la pale, la vitesse dans le sens de l'envergure est faible lorsque la couche limite est attachée. En conséquence, la transition naturelle est très similaire au profil 2D et est aux ondes de Tollmien – Schlichting (TS). Sur la pale d'hélice marine, l'écoulement de la couche limite est entièrement tridimensionnel (3D) en raison de la rotation. L'instabilité et la transition des "cross-flow" sont clairement observées. La forme des tourbillons est en bon accord avec la prédiction de la théorie de la stabilité linéaire (LST). Bien qu'il ait été longtemps supposé que la "cross-flow" transition devrait être importante sur les hélices, il s'agit de la première observation directe de tels phénomènes à notre connaissance. Parce que l'hélice n'a pas de symétrie de rotation infinie, notre résultat suggère que la couche limite sur les hélices marines est instable par convection. Cet aspect est différent par rapport a l'écoulement de von Kármán, qui est inconditionnellement instable
The boundary layers on HAWTs and marine propellers share an apparent common point with von Kármán swirling flow, which is created by a rotating disk in the otherwise still fluid. von Kármán swirling flow is the prototype of cross-flow transition. Therefore one focus of the present study is the possibility of cross-flow transition on HAWTs and marine propellers. This study shows that the natural boundary layer transitions on the HAWT and the marine propeller are induced by distinctively different mechanisms. The numerical result of a HAWT blade shows that the boundary layer profile on it is very close to 2-Dimensional (2D) airfoil flow. On the blade, the velocity in spanwise direction is small in the attached boundary layer. As a result, the natural transition on HAWT blade is very similar to the 2D airfoil and is due to Tollmien-Schlichting (TS) wave. On the marine propeller blade, the boundary layer flow is fully 3-Dimensional (3D) due to rotation. Cross-flow instability and transition are clearly observed. The shapes of the cross-flow vortices are in good agreement with the prediction of Linear Stability Theory (LST). Although its been long assumed that cross-flow transition should be important for propellers, this is the first direct observation of such phenomena as far as we know. Because the propeller does not have infinite rotational symmetry, our result suggests the boundary layer on the marine propeller is convectively unstable. This is different with von Kármán boundary layer flow, which is absolutely unstable
APA, Harvard, Vancouver, ISO, and other styles
17

Keenan, David P. "Marine propellers in unsteady flow." Thesis, Massachusetts Institute of Technology, 1989. http://hdl.handle.net/1721.1/14348.

Full text
APA, Harvard, Vancouver, ISO, and other styles
18

Jastram, Michael Oliver. "Inspection and feature extraction of marine propellers." Thesis, Massachusetts Institute of Technology, 1996. http://hdl.handle.net/1721.1/42632.

Full text
APA, Harvard, Vancouver, ISO, and other styles
19

Güner, Mesut. "A rational approach to the design of propulsors behind axisymmetric bodies." Thesis, University of Newcastle upon Tyne, 1994. http://hdl.handle.net/10443/3118.

Full text
Abstract:
In the context of "Lifting Line Methodology", this thesis presents a rational approach to Marine Screw Propeller design and its applications in combination with a "Stator" device for further performance improvement. The rational nature of the approach is relative to the Classical Lifting Line procedure and this is claimed by more realistic representation of the propeller slipstream tube which contracts in radial direction along the tube at downstream. Therefore, in accordance with the Lifting Line Methodology, the design procedure presented in this thesis involves the representation of the slipstream shape by a trailing vortex system. The deformation of this system is considered by means of the so-called "Free Slipstream Analysis Method" in which the slipstream tube is allowed to deform and to align with the direction of local velocity which is the sum of the inflow velocity and induced velocities due ,to the trailing vortices. This deformation is neglected in the Classical Lifting Lin~ approach. The necessary flow field data or the wake for the design is predicted by using a three-dimensional "Panel Method" for the outer potential flow, whilst a "Thin Shear Layer Method" is used for the inner boundary layer flow. The theoretical procedures in both methods neglect the effect of the free surface and therefore the implemented software for the flow prediction caters only for deeply submerged bodies. However, the overall design software is general and applicable to surface ships with an external feedback on the wake. Since the realistic information on the slipstream shape is one of the key parameter in the design of performance improvement devices, the proposed design methodology has been combined with a stator device behind the propeller and the hydrodynamic performance of the combined system has been analysed. The design analysis involved the torque balancing characteristics of the system and the effects of systematic variations of the key design parameters on the performance of torpedo shape bodies and surface ships at varying loading conditions. The ·overall conclusions from the thesis indicate that a more realistic representation of the slipstream shape presents a higher efficiency in comparison to the regular slipstream shape assumption, in particular for heavily loaded propellers. Moreover, this representation is essential for sound design of the stator devices as it will determine the radius of the stator. From the investigation on the stator it was found that the undesirable effect of the unbalanced propeller torque can be avoided by the stator. The efficiency of the system will increase with the increase in the number of stator blades and the distance between the stator and the propeller over a practical range of the design parameters. It is believed that the procedure and software tool provided in this thesis could provide the designer with capability for more sound propeller and the stator design for, partly, surface ships and for submerged ships in particular torpedos, Autonomous Underwater Vehicles (AUV) and submarines. Although the improvement gained by the present procedure will be accompanied by an increase in computer time, this is not expected to be a major problem considering the enormous power of existing computers. In fact, this has been the major source of encouragement for the recommendation in this thesis to improve the present procedure by using the "Lifting Surface Methodology" as the natural extension of the Lifting Line Methodology.
APA, Harvard, Vancouver, ISO, and other styles
20

Mulcahy, Norman Lex Mechanical &amp Manufacturing Engineering Faculty of Engineering UNSW. "Structural design of shape-adaptive composite marine propellers." Awarded By:University of New South Wales. Mechanical & Manufacturing Engineering, 2010. http://handle.unsw.edu.au/1959.4/44629.

Full text
Abstract:
Nickel-Aluminium-Bronze alloy is the most common material for ship propellers but, more recently, composite materials have been used in propeller construction. One of the advantages of the use composite materials for ship propellers is that they allow the possibility of shape-adaptability. A shape-adaptive propeller is one that is designed so that the blades deform with load changes in such a way that the propeller performance is enhanced in comparison to that of a conventional ??rigid?? propeller, e.g. the goal of shape-adaptability may be higher efficiency over a greater range of operating conditions, or reduced cavitation and noise. This shape-adaptability can be achieved through the choice of the appropriate blade geometry, and the optimum arrangement of composite materials. A design method for composite shape-adaptive propellers is developed and tested in this work. The method has a baseline rigid propeller as the starting point. A novel method is used to identify a design condition at which the rigid and flexible propellers have identical shapes, and therefore performance. Optimisation procedures, to find the unloaded shape and composite material properties, are a necessary part of the shape-adaptive propeller design method. A shape-adaptive flexible propeller has generally improved performance compared to that of the baseline rigid propeller. As well, a coupled hydrodynamic/structural analysis is required so that the performance of flexible and rigid propellers can be compared. The results of a study of the twist characteristics of straight and curved cantilever beams with various amounts of skew are reported. The cantilever beams are structural analogues of hydrofoils and propeller blades, and the aim of the study is to identify the desired material and geometrical characteristics for shape-adaptive propellers and hydrofoils. Two case studies, that demonstrate the developed design procedures, are described: Design of a flexible hydrofoil, and Design of a flexible propeller. In both cases, the desired shape-adaptive behaviour is achieved but the performance gains are small. It is felt that the example structures do not have sufficient flexibility to take full advantage of shape-adaptability. Possible means of achieving greater flexibility are optimisation of the baseline shape (planform and thickness distribution) for flexibility, and selection of composite materials that maximise flexibility, within the strength requirements. An expression is developed for estimating the efficiency gain of a shape-adaptive propeller operating at the design condition in a ship??s wake. Calculations show that, even for what is considered to be a relatively flexible propeller, the expected efficiency gains are small (< 1%). However, small gains in efficiency across the range, can be significant for the operation of a ship. Furthermore, efficiency gains are higher at off-design conditions as a shape-adaptive design broadens the efficiency curve.
APA, Harvard, Vancouver, ISO, and other styles
21

Roddis, Mark Edward. "On the inverse design of marine ducted propulsor blading." Thesis, University College London (University of London), 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.265865.

Full text
APA, Harvard, Vancouver, ISO, and other styles
22

Califano, Andrea. "Dynamic loads on marine propellers due to intermittent ventilation." Doctoral thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for marin teknikk, 2010. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-11789.

Full text
Abstract:
Dynamic Positioning (DP) systems are increasingly replacing traditional positionkeeping methods—such as jack-up barges and anchoring systems—on board ships operating in ever deeper waters. During these operations, the combined effect of heavy sea states and high propeller loadings have caused a number of damages on azimuth and tunnel thrusters, causing service downtime and requiring costly repairs. Damages in rough seas were reported also during transit operations. These damages can be caused by dynamic loads on the propeller due to intermittent ventilation. Ventilation occurs on thrusters operating at high loadings and low submergence, experiencing continuous cycles in- and out-of water. This leads to sudden thrust losses and violent impact loads. The present work aims at modeling the dynamic loads during propeller ventilation, in order to predict the corresponding losses. Model tests and numerical simulations were performed in order to better understand the mechanisms of dynamic forces due to ventilation. Furthermore, numerical simulations carry on the challenge of applying a Volume of Fluid (VOF) method to this type of problem. The performed model tests have shown two main ventilation mechanisms, depending on the propeller submergence, loading and advance ratio: (i) at deeper submergence through a free-surface vortex and (ii) at moderate submergences through the blade itself piercing the free surface. These two mechanisms can exist separately or at the same time, identifying three distinctive ventilation regimes. The performed numerical simulations are able to reproduce the main features observed during the experiments: air is drawn from the free-surface and transported along the propeller rotation, for both the ventilation types previously identified. The dynamic loads computed with the numerical model are in satisfactory agreement with the experimental data at the upright position where the blade is piercing the free-surface, whereas thrust is over-estimated at all the other angular positions. Unlike ventilation of surface-piercing propellers with super-cavitating profile, it was found that the tip-vortex has a dominant role in the type of ventilation object of this study. The tip-vortex was also identified as the most likely factor responsible for the overestimation found in the numerical simulations of the thrust for the angular positions where the blade is deeply submerged. Other causes for the deviation between numerical simulations and experiments are further discussed. A qualitative model of the dynamic loads occurring during one propeller revolution was derived, based on the impact of the blade with the air entrained by the tip vortex, leading to two main thrust losses: (i) an absolute minimum loss about the angular position of π/4 and (ii) a local minimum loss about 3/2π.
APA, Harvard, Vancouver, ISO, and other styles
23

Smogeli, Øyvind Notland. "Control of Marine Propellers : from Normal to Extreme Conditions." Doctoral thesis, Norwegian University of Science and Technology, Department of Marine Technology, 2006. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-1463.

Full text
Abstract:

This is a thesis about control of marine propellers. All ships and underwater vehicles, as well as an increasing number of offshore exploration and exploitation vessels, are controlled by proper action of their propulsion systems. For safe and cost effective operations, high performance vessel control systems are needed. To achieve this, all parts of the vessel control system, including both plant level and low-level control, must be addressed. However, limited attention has earlier been given to the effects of the propulsion system dynamics. The possible consequences of improper thruster control are:

• Decreased closed-loop vessel performance due to inaccurate thrust production

• Increased vessel down-time and maintenance cost due to unnecessary mechanical wear and tear.

• Increased fuel consumption and risk of blackouts due to unpredictable power consumption.

By focusing explicitly on the propeller operating conditions and the available options for low-level thruster control, this thesis presents several results to remedy these problems.

Two operational regimes are defined: normal, and extreme conditions. In normal operating conditions, the dynamic loading of the propellers is considered to be moderate, and primarily caused by oscillations in the inflow. In extreme conditions, the additional dynamic loads due to ventilation and in-and-out-ofwater effects can be severe. In order to improve the understanding of these loads and develop a simulation model suitable for control system design and testing, systematic model tests with a ventilating propeller in a cavitation tunnel and a towing tank have been undertaken.

In conventional propulsion systems with fixed-pitch propellers, the low level thruster controllers are usually aimed at controlling the shaft speed. Other control options are torque control and power control, as well as combinations of the three. The main scientific contributions of this thesis are:

• A combined torque/power controller and a combined speed/torque/power controller are designed. When compared to conventional shaft speed control, the proposed controllers give improved thrust production, decreased wear and tear, and reduced power oscillations.

• A propeller load torque observer and a torque loss estimation scheme is developed, enabling on-line monitoring of the propeller performance.

• An anti-spin thruster controller that enables use of torque and power control also in extreme operating conditions is motivated and designed. By applying the load torque observer to detect ventilation incidents, the antispin controller takes control of the shaft speed and lowers it until the ventilation incident is terminated.

• A propeller performance measure that can be used to improve thrust allocation in extreme operating conditions is introduced.

The proposed controllers and estimation schemes are validated through theoretical analyses, numerical simulations, and experiments on a model-scale propeller.

APA, Harvard, Vancouver, ISO, and other styles
24

Jinkerson, Richard Alan. "Constrained and unconstrained localization for automated inspection of marine propellers." Thesis, Monterey, California. Naval Postgraduate School, 1991. http://hdl.handle.net/10945/25782.

Full text
APA, Harvard, Vancouver, ISO, and other styles
25

Searle, Timothy John. "The manufacture of marine propellers in moulded anisotropic polymer composites." Thesis, University of Plymouth, 1998. http://hdl.handle.net/10026.1/2766.

Full text
Abstract:
This thesis examines the feasibility of manufacturing small marine propellers from continuous fibre reinforced polymer composite materials. An appraisal of some current applications of composite materials in the marine industry is given, together with the moves shown towards the use of composites in the area of propeller design. It has been shown that manufacturing propellers in composite materials is theoretically more cost effective than traditional materials. The manufacturing route investigated is Resin Transfer Moulding, where some detailed investigations have highlighted some of the critical processing parameters necessary for successful production of laminates suitable for propellers and other high performance marine structures. A thorough testing programme of 4 novel designs of composite propeller is reported. Trials at sea on university run vessels has enabled many hours use to be logged, which has shown the fitness for purpose of propellers made from glass reinforced, epoxy composite. Experimental tank testing has helped to shape the remainder of the research by identifying the possibility of using hydroelastic tailoring to improve the efficiency of the propeller when a variety of operating conditions are required from the propulsion system. Further experience is required with respect to the the tooling construction and the life assessment of the propeller. To facilitate appropriate modelling of the propeller, spreadsheet based load prediction models have been used. Finite element analysis (FEA) was used to model the elastic characteristics of one particular design of novel composite propeller. This indicated that traditional geometries may be too stiff to allow significant performance advantages from the anisotropy of the material. However the potential does exist for modified propeller geometries made from composite to give some performance benefit. For specific applications, small marine propellers made from continuous glass fibre reinforced epoxy composite are likely to yield cost savings over traditional propeller materials.
APA, Harvard, Vancouver, ISO, and other styles
26

Hufford, Gary S. (Gary Scott). "Viscous flow around marine propellers using boundary layer strip theory." Thesis, Massachusetts Institute of Technology, 1992. http://hdl.handle.net/1721.1/42543.

Full text
APA, Harvard, Vancouver, ISO, and other styles
27

Pivano, Luca. "Thrust Estimation and Control of Marine propellers in Four-quadrant Operations." Doctoral thesis, Norwegian University of Science and Technology, Department of Engineering Cybernetics, 2008. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-2124.

Full text
Abstract:

Speed and position control systems for marine vehicles have been subject to an increased focus with respect to performance and safety. An example is represented by drilling operations performed with semi submersible rigs where the control of position and heading requires high accuracy. Drifting from the well position could cause severe damage to equipment and environment. Also, the use of underwater vehicles for deep ocean survey, exploration, bathymetric mapping and reconnaissance missions, has become lately more widespread. The employment of such vehicles in complex missions requires high precision and maneuverability.

This thesis focuses on thrust estimation and control of marine propellers with particular attention to four-quadrant operations, in which the propeller shaft speed and the propeller inflow velocity (advance speed) assume values in the whole plane. In the overall control system, propellers play a fundamental role since they are the main force producing devices. The primary objective of the thruster controller is to obtain the desired thrust from the propeller regardless the environmental state. During operations, propellers are often a¤ected by thrust losses due to e.g. changes in the in-line water velocity, cross flows, ventilation, in-and-out of water effects, wave-induced water velocities, interaction between the vessel hull and the propeller and between propellers. Propellers may thus work far from ideal conditions. Therefore, the knowledge of the propeller thrust and torque, together with forces induced by the interaction between the vehicle and propellers and between propellers, is fundamental to achieve high control performance. Unfortunately a propeller system is usually not equipped with thrust and torque sensors, therefore thrust losses are not directly measured.

Motivated by this, a new four-quadrant thrust estimation scheme is presented, extending previous results valid for propeller operating in two quadrants. Based on shaft speed and motor torque measurements, the scheme involves a nonlinear observer for the propeller torque that shows stability and robustness for bounded modeling and measurement errors. The propeller thrust is computed as a static function of the propeller torque. The performance is demonstrated in experimental tests, showing improved accuracy in the thrust reproduction with respect to the direct use of the four-quadrant propeller characteristics.

A nonlinear observer for the torque loss estimation, similar to the one implemented in the thrust estimation scheme, is included in a new fourquadrant nonlinear thrust controller, designed for calm and moderate sea conditions. The control strategy is based on a shaft speed controller where the desired velocity is computed from the desired propeller thrust and on the torque losses. Experimental results are provided, demonstrating the e¤ectiveness of the new controller with respect to the conventional shaft speed and torque controllers.

The thrust controller, designed for calm and moderate sea conditions, is subsequently improved by including an anti-spin strategy to reduce power peaks and wear-and-tear in extreme sea conditions. The anti-spin strategy is derived from previous works that were designed for Dynamics Positioning (DP) operations. The presented controller can operate also for maneuvering and transit operations, where the vehicle speed is larger than in DP operations. The performance of the controller is validated by experimental tests.

Motivated by environmental issues and the need of reduced fuel consumption and CO2 emissions, a novel control scheme for improving, in moderate sea, the propulsion e¢ ciency with respect to conventional propeller controllers is presented. The main idea is to exploit the variation in the advance speed due to waves to increase the average propulsion efficiency without reducing the vessel speed. A nonlinear controller is proposed showing that, theoretically, is possible to increase the propulsion efficiency. Model tests determine dynamic characteristics of propellers in waves and a simulation is employed to validate the novel control scheme.

APA, Harvard, Vancouver, ISO, and other styles
28

Aktas, Batuhan. "A systematic experimental approach to cavitation noise prediction of marine propellers." Thesis, University of Newcastle upon Tyne, 2017. http://hdl.handle.net/10443/3639.

Full text
Abstract:
Minimization of propeller cavitation noise is best achieved through accurate and reliable pre-dictions at an early design stage. The effect of cavitation and particularly the dynamics of cav-itation on URN is rather complex to understand and the current state of the art does not offer a plausible cavitation noise prediction method which can be implemented within the propeller design spiral. Within this framework, the aim of the present thesis is to enhance the understand-ing of the propeller cavitation noise by conducting detailed systematic cavitation tunnel tests to investigate the main propeller design parameters and operating conditions and to scrutinize their impact on propeller Radiated Noise Levels (RNL). The resulting experimental data are also utilized to compile a database that enables engineering a novel noise prediction method to be developed and used at preliminary design stage, using standard series approach. A holistic approach to cavitation noise has been adopted through experimental investigations into oblique flow effects on propeller noise and by conducting full scale and model scale noise experiments of a research vessel. These have been used to evaluate the capabilities of the adopted standard series based experimental prediction methodology. The accumulated knowledge based on prior experiments has been utilized to design standard series propeller test campaign. Experiments using members of Meridian standard propeller se-ries were tested both in an open water condition and also behind systematically varied wake inflows. Initially, a small subset of the Meridian standard propeller series was chosen, with loading conditions derived from in-service, ocean-going vessels. The resulting measured noise data were extrapolated to full-scale based on the powering information of these vessels to com-pare with average shipping noise data. Finally, a larger subset of the propeller series was tested systematically to compile a database of propeller cavitation noise and for the development of noise prediction software.
APA, Harvard, Vancouver, ISO, and other styles
29

Pontarelli, Matthew. "Flow regimes and instabilities of propeller crashback." Thesis, University of Iowa, 2017. https://ir.uiowa.edu/etd/5826.

Full text
Abstract:
Crashback operation of a propeller is a common emergency slowing maneuver for ships and submarines. The reversing of the propeller while the vessel is moving forward results in large loads on the propeller blades and highly detached flow, which presents both practical concerns and fundamental fluid physics inquiries. This thesis contains a comprehensive numerical analysis of two propellers in crashback operation. Available numerical and experimental data for David Taylor Model Basin (DTMB) 4381 propeller are used for validation of the computational fluid dynamics solver used, REX. A second propeller, Maritime Research Institute Netherlands (MARIN) 7371R is used to classify the common crashback flow behavior into regimes. Four regimes were identified, each existing for a range of operating conditions. The most prominent and deciding feature of the flow regimes is the presence of a ring vortex, resulting from the opposing action of the free-stream flow and the propeller induced flow. The position, shape and strength changes between regimes, dominating the dynamics of the flow by altering the induced flow into the propeller disk. Flow conditions resulting from regime transitions are described. Changes in the ring vortex structure lead to two stable flow conditions of interest. One condition produces a reduction of thrust despite the increase in flow speed into the propeller and negligible side-forces. The other condition creates large side-forces capable of rotating a vessel, resulting from an asymmetry forming in the ring vortex. Additionally, massive flow separation occurs at high free-stream speeds that cause extreme blade loading. An extensive description of each flow regime is provided, with further investigation and discussion of the flow regimes that present more practical concerns and novel characteristics of the crashback flow.
APA, Harvard, Vancouver, ISO, and other styles
30

Aryawan, Wasis Dwi. "An investigation into the potential of multiple rows ducted propellers for marine applications." Thesis, University of Newcastle Upon Tyne, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.275427.

Full text
APA, Harvard, Vancouver, ISO, and other styles
31

Korkut, Emin. "An investigation into the scale effects on cavitation inception and noise in marine propellers." Thesis, University of Newcastle Upon Tyne, 1999. http://hdl.handle.net/10443/1135.

Full text
Abstract:
This thesis presents an investigation into the phenomena of scale effects on cavitation inception and noise of marine propellers. The overall aim is to extend the understanding of these phenomena and improve predicting methods. The investigations, which are largely experimental in nature, are restricted to the tip vortex and sheet types of cavitation. Chapter 1 includes a state-of-the-art review of the scale effect studies based on published papers to form the basis for the main objectives and structure of thesis. The objectives require systematic tests in a cavitation tunnel to explore the viscous scale effects contributing to the phenomena, particularly for the effect of the free-stream turbulence, and to include this effect in extrapolation procedures. Chapter 2 is concernedw ith the background flow measurementsin the cavitation tunnel under the effect of systematically varying levels of the free-stream turbulence generated by using wire meshes. This background information is obtained using a Laser Doppler Anemometry; measurements made with the latter provide a systematic basis on which the analyses of the cavitation inception and noise experiments can be performed. In Chapter 3, a set of cavitation inception tests is described with a NACA66 rectangular foil whose cross-section represents a typical blade section of a marine propeller. The inception measurements for systematically varying levels of the free-stream turbulence and that of the leading edge roughness are presented for different angles of attack and the results are discussed. Chapter 4 includes another set of cavitation inception experiments with a 5-bladed of model propeller of the Meridian Series. The measurements are taken for varying levels of the free-stream turbulence, blade roughness and dissolved gas contents. The results are analysed and discussed with a specific emphasis on the similarities between the effects of the free-stream turbulence and blade roughness. Chapter 5 presents a set of systematic noise measurements, with the same test propeller under the similar effects of the free-stream turbulence, blade roughness and dissolved gas content, using a single external hydrophone. The analyseso f these measurements,in terms of the tunnel background noise and net propeller noise, are presented and discussed for two operating conditions representing a typical non-cavitating and cavitating noise spectrum. In Chapter 6, a semi-empirical tool is developed to predict the inception of cavitation including the effect of the free-stream turbulence based on Lighthill's Leading Edge Correction factor (Lighthill, 1951). This tool is correlated with the inception tests results of the model propeller and its potential to be used as an extrapolator for the full-scale prediction is discussed. An attempt is made to establish a correspondence between the level of the free-stream turbulence and that of the blade roughness and its impact on the current test procedures is discussed. This chapter also includes an analysis of the similarity criteria to incorporate the effect of the free-stream turbulence in the inception of cavitation using the Dimensional Analysis procedure. In Chapter 7, a general review of the study together with the main conclusions from the thesis are presented and some recommendations for future work are made.
APA, Harvard, Vancouver, ISO, and other styles
32

Prasetyawan, Ika. "On the use of B-spline technique in geometry and hydrodynamics of marine propellers." Thesis, University of Newcastle Upon Tyne, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.275522.

Full text
APA, Harvard, Vancouver, ISO, and other styles
33

Lee, Jintae. "A potential based panel method for the analysis of marine propellers in steady flow." Thesis, Massachusetts Institute of Technology, 1987. http://hdl.handle.net/1721.1/14641.

Full text
APA, Harvard, Vancouver, ISO, and other styles
34

Webster, John Ackroyd III. "Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling." Diss., Virginia Tech, 2019. http://hdl.handle.net/10919/93038.

Full text
Abstract:
Small-scale marine propellers operate at low Reynolds numbers, where laminar-turbulent transition of the boundary layer can impact the distributions of pressure and shear stress on the blade surface. Marine propellers operating at low Reynolds numbers are subject to laminar-turbulent transition of the boundary layer, which impacts the distributions of pressure and shear stress on the blade surface. To design efficient propellers for operation at low Reynolds numbers, transitional effects must be included in the evaluations of propeller performance. In this work, transition modeling techniques in Reynolds Averaged Navier- Stokes computational fluid dynamics (RANS CFD) are utilized to evaluate and design propellers operating at low Reynolds numbers. The Galilean invariant γ transition model with an extension for crossflow transition is coupled to the SSG (Speziale, Sarkar, Gatski) /LRR (Launder, Reece, Rodi) -ω Reynolds stress transport turbulence model, with validation cases performed for flate plate boundary layers, 2-dimensional airfoils, a 3-dimensional wing, and 6:1 prolate spheroids. The performance of the coupled SSG/LRR-ω-γ Reynolds stress transition model for propellers with flow transition is then evaluated using experimental surface streamline and force data from four model-scale marine propellers. A method for the design of low Reynolds number marine propellers is presented using a transition-sensitive lifting line method coupled with the panel method code XFOIL. Initial geometries generated using the lifting-line method are then optimized in RANS CFD using the 2 equation γ-Reθ transition model and an adjoint method to warp the propeller shape to improve the efficiency. Two design studies are performed, including an open water propeller, and a propeller designed for a small autonomous underwater vehicle.
Doctor of Philosophy
Small-scale marine propellers exhibit transition from laminar to turbulent flow in the region near the surface of the blades. Regions of laminar and turbulent flow on the blade surface contribute differently to the overall thrust and torque on the propeller. Prediction of flow transition in the design process for small-scale marine propellers can improve the accuracy of the thrust and torque prediction compared to modeling the flow as purely laminar or turbulent. Propeller thrust and torque can be modeled using computational fluid dynamics (CFD) simulations, where transition modeling is accomplished by solving a transport equation for the intermittency γ, which represents the percentage of time the flow in a given location is turbulent. In this work, a transition model is coupled to a high-fidelity full Reynolds stress turbulence model, which solves 6 transport equations to solve for each component of the Reynolds stress tensor. The Reynolds stress tensor represents the turbulent velocity fluctuations in the governing equations solved in the CFD simulation. This coupled transition and turbulence model is then validated using experimental results of flows with a number of different transition mechanisms. The coupled model is then tested with a series of model-scale propellers, with results of the CFD simulations compared to the experimental results. A method for the design of propellers with flow transition is presented which incorporates transition effects. The designs generated by this method are then optimized in a CFD framework which morphs the blade geometry to improve the ratio of the thrust produced by the propeller to the torque, which corresponds to a higher efficiency. Two design cases are presented: a propeller designed for open water operation, and a propeller design for a small autonomous underwater vehicle.
APA, Harvard, Vancouver, ISO, and other styles
35

Lidtke, Artur K. "Predicting radiated noise of marine propellers using acoustic analogies and hybrid Eulerian-Lagrangian cavitation models." Thesis, University of Southampton, 2017. https://eprints.soton.ac.uk/413579/.

Full text
Abstract:
Anthropogenic noise from a variety of merchant ships has been reported to be a major factor adversely aecting marine organisms. Consequently, scientists and regulators have become more vocal about encouraging, and possibly enforcing, quieter ships in the future. For this to be feasible from an engineering standpoint, a range of numerical methods must be made available to allow acoustic performance of vessels to be evaluated at the design stage. Cavitation is a major contributor to the hydroacoustic signature of a merchant vessel. The reason for this is the relatively high drop of pressure induced by the propeller, which in turn promotes the growth of vapour bubbles and cavities, oscillation and collapse of which act as strong acoustic sources. The entire process is made more dynamic by the non-uniform wake of the ship, propeller rotation, as well as the fact that vessels travel in a seaway. Because of its complexity, the problem of marine propeller noise is thus not widely studied numerically, which translates to the lack of tools readily available to designers willing to reduce the noise generated by ships. A set of numerical utilities are proposed which could be employed at the late design stage of a merchant ship in order to allow the designer to estimate the radiated noise and make informed decisions on how to improve the design. The methodology involves solving the turbulent flow over the propeller using Detached Eddy Simulation (DES) and modelling cavitation using a mass-transfer model. The porous Ffowcs Williams-Hawkings acoustic analogy is used to infer far-eld radiated noise caused by the blade rotation, pulsating cavitation, as well as non-linear noise sources in the propeller slip-stream. The cavitation model is also extended to incorporate Lagrangian bubbles dispersed downstream of the large cavities modelled using the baseline Schnerr-Sauer model via the volume fraction equation approach. This allows the broadband nature of cavitation noise to be captured. The methods are applied to a NACA 66 and the Delft Twist 11 hydrofoil test cases. Although there are limited validation data allowing all of the methods to be validated simultaneously, relatively good agreement is seen at intermediate validation stages. These include comparing the non-cavitating noise of the Insean E779a propeller to reference data, conducting acoustic predictions for idealised acoustic sources, as well as comparing cavitation patterns, cavity cloud shedding frequencies, and induced pressures to experimental data for hydrofoils and propellers. It is concluded that the presented methodology may be used to predict low-frequency noise due to cavitation in a relatively robust manner, although the method is yet to be tested and validated on more complex geometries. The hybrid Eulerian-Lagrangian model is still at an early stage and a range of areas for improvement have been identified, such as implementation of more realistic cavity break-up models as well as better coupling between the fluid and bubble solvers. Nonetheless, the method is demonstrated to be a promising tool at tackling the broadband cavitation noise components as it can capture the contribution of the mass of small, oscillating bubbles on the radiated pressure which would otherwise be unaccounted for in the baseline Eulerian framework.
APA, Harvard, Vancouver, ISO, and other styles
36

Epps, Brenden P. "An impulse framework for hydrodynamic force analysis : fish propulsion, water entry of spheres, and marine propellers." Thesis, Massachusetts Institute of Technology, 2010. http://hdl.handle.net/1721.1/61519.

Full text
Abstract:
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2010.
This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
Cataloged from student-submitted PDF version of thesis.
Includes bibliographical references.
This thesis presents an impulse framework for analyzing the hydrodynamic forces on bodies in flow. This general theoretical framework is widely applicable, and it is used to address the hydrodynamics of fish propulsion, water entry of spheres, and the offdesign performance of marine propellers. These seemingly-unrelated physics problems share a key common thread: The forces on these fish, spheres, and propellers can be modeled as the sum of the reaction to the rate of change of (1) the pressure impulse required to set up the potential flow about the body, and (2) the vortex impulse required to create the vortical structures in the wake of the body. Fish generate propulsive forces by creating and manipulating large-scale vortical structures using their body and tail. High-speed particle image velocimetry experiments show that a fish generates two vortex rings during a C-turn maneuver and that the change in momentum of the fish balances the change in pressure impulse plus the vortex impulse of these rings. When a sphere plunges into a basin of water and creates a sub-surface air cavity in place of a vortical wake, the vortex impulse is zero, and the force on the sphere is given by the pressure impulse component. Using data from high-speed imaging experiments, a semi-empirical numerical simulation is developed herein; this numerical model shows how the presence of the cavity alters the unsteady pressure force on the sphere and modulates the dynamics of the impact event. During steady propeller operation, the pressure impulse is constant, and the loads on the propeller are given by the vortex impulse component. To analyze these loads, a computational design and analysis tool is presented; this code suite is based on propeller lifting line theory, which is shown to be a special case of the general impulse framework of this thesis. A marine propeller is designed, built, and tested over a range of off-design operating conditions. Experimental results match the predicted performance curve for this propeller, which provides important validation data for the numerical method presented herein. 3 Bringing this thesis full circle, the unsteady startup of the propellor is addressed, which is analogous to the impulsive maneuvering of the swimming fish. As in the fish maneuvering problem, the propellor generates a ring-like vortical wake, and it is shown herein how the vortex impulse of these rings provides thrust for the propellor. With the perspective of the impulse framework developed in this thesis, the results of these tandem experimental investigations and numerical simulations provide deeper insight into classical fluid-dynamics theory and modern experimental hydrodynamics.
by Brenden P. Epps.
Ph.D.
APA, Harvard, Vancouver, ISO, and other styles
37

Diniz, Giovani. "A fully numerical lifting line method for the design of heavily loaded marine propellers with rake and skew." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/100140.

Full text
Abstract:
Thesis: S.M. in Naval Architecture and Marine Engineering, Massachusetts Institute of Technology. Department of Mechanical Engineering, 2015.
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 85-86).
This thesis aims to give a contribution to the design of heavily loaded marine propellers by numerical methods. In this work, a wake-adapted, fully numerical, lifting line model is used to obtain the optimum circulation distribution along the propeller's blade via variational method, presented by Coney [9]. In this context, two approaches to the representation of the wake field are compared: the first approach utilizes Betz's condition for moderately loaded propellers, in which the wake is aligned with the hydrodynamic pitch angle. The second approach, in which the wake is aligned with the local velocities, utilizes Kutta's Law to create a zero-lift wake surface. A thorough comparison of the influence of the effect of tip vortex roll-up is done. A lifting surface method with fully aligned wake is developed and used to correct the optimum distribution of pitch and camber obtained by the new lifting line method. The resulting geometries, operating under heavily-loaded conditions, are submitted to a preliminary analysis in a boundary element-based potential flow code to verify the consistency of the results. This analysis confirms the better results obtained with the fully numerical lifting line model and the variations between the approaches in terms of circulation and pitch angle observed in the lifting line results are verified. Finally, the performance of propeller geometries generated with the approaches studied in this work are compared by high fidelity RANSE analysis. The CFD simulations confirm the higher accuracy of the method in which the wake geometry is aligned with the local velocities in terms of fulfillment of thrust requirement.
by Giovani Diniz.
S.M. in Naval Architecture and Marine Engineering
APA, Harvard, Vancouver, ISO, and other styles
38

Tonacio, Victor Coracini. "Avaliação de propulsores navais em relação a eficiência e excitação de vibração." Universidade de São Paulo, 2013. http://www.teses.usp.br/teses/disponiveis/3/3135/tde-21102014-112150/.

Full text
Abstract:
A escolha do propulsor é uma etapa-chave no projeto de um navio. Muito do que se espera qualitativamente do desempenho de uma embarcação implica em economia de energia, em condições de operação e habitabilidade adequadas à tripulação, e em baixo custo de manutenção dos elementos estruturais e dos equipamentos. Essas questões estão diretamente relacionadas ao aproveitamento de combustível pelo sistema propulsivo e à propagação de vibração, cabendo ao propulsor um papel significativo para a performance do navio em ambos os aspectos. Por esta razão, a dissertação propõe a avaliação de propulsores navais com respeito à excitação de vibração e à eficiência, quando atuando em esteira não uniforme. A dissertação inicia-se com uma abordagem resumida especificamente sobre os estudos já realizados sobre indução de vibração pelo propulsor focados nas chamadas forças de mancal. Em seguida, revisam-se os assuntos pertinentes ao projeto de propulsor, isto é, definição de sua geometria, de seus coeficientes de operação, e dos métodos teóricos e computacionais utilizados para estudar seu comportamento hidrodinâmico. A metodologia do trabalho fundamenta-se no estudo paramétrico da geometria do hélice, objetivando identificar a influência de cada um dos parâmetros de projeto do propulsor nos dois aspectos destacados no início. As diversas configurações geométricas são submetidas a campos de velocidades advindos de diferentes navios, que representam três grupos de embarcações (navios série 60, porta-containers e navios-tanque), com o intuito de verificar as diferentes tendências de comportamento possíveis. Para a execução computacional, elabora-se uma rotina encarregada de sistematizar o processo de alterações geométricas, encaminhar os numerosos casos à análise hidrodinâmica, realizar o processo de integração casco-hélice e o pós-processamento dos resultados. A análise hidrodinâmica citada é feita através do uso de um software comercial, que, baseado na teoria do escoamento potencial, aplica o método dos painéis para a resolução do escoamento ao redor do propulsor. Os esforços excitados pelo hélice são traduzidos em critérios objetivos, baseados na transmissão de vibração através do eixo, que, associados ao critério de eficiência propulsora e à restrição relativa à ocorrência de cavitação, avaliam os casos e identificam-se o comportamento dos parâmetros de projeto. Obtém-se, como conclusão, uma metodologia de avaliação aplicável em outros casos de propulsores e navios.
The propeller choice is a key-step of the ship design. The high quality of the vessel performance requires energy economy, appropriated operating and environmental conditions for the crew, and low maintenance costs of structural elements and equipment. These questions consider directly fuel consumption by the propulsion system and the transmitted vibration, regarding the propeller an important role in the ships performance about both attributes. For this reason, the evaluation of marine propellers, regarding the induced vibration and the propulsive efficiency under a non-uniform inflow, is proposed. The study begins with a briefly state of the art about the propeller induced vibration focused in bearing forces. Then, a propeller design overview is made about subjects such as geometry definition, operation coefficients, and theoretical and computed methods for studying its hydrodynamic behavior. The methodology is based on a parametric study of the propeller geometry, in order to identify the influence of each of the propeller design parameters in both aspects highlighted in beginning. The several geometric configurations are submitted to the wake fields from different ships, that represent three groups of vessels (60 series, containers and tankers), then different tendencies of behavior can be expected. For computational execution, a routine is in charge of systematizing the process of geometrical parameterization, send the cases to the hydrodynamic analysis, make the hull-propeller integration and post process the data. The hydrodynamic analysis is compelled by a HSVA® software, which applies the panel method in the propeller flow, based on potential flow theory. The propeller induced bearing forces are converted in objective criteria, based on vibration transmission through the shaft, which, combined with the propulsive efficiency criteria and the cavitation restriction, evaluate the propeller geometric configurations. As a conclusion, a propeller evaluation methodology applicable to another kind of propeller series and wake fields is obtained.
APA, Harvard, Vancouver, ISO, and other styles
39

Berg, Magnus. "Nanostrukturell ytbeläggning på utsatta delar av marina drivlinor." Thesis, Försvarshögskolan, Militärtekniska avdelningen (MTA), 2010. http://urn.kb.se/resolve?urn=urn:nbn:se:fhs:diva-977.

Full text
Abstract:
Nowadays naval units are participating in international missions, where new and in many cases tougher conditions will affect their propulsion.   This essay deals with some of the now developed nanostructure coatings and gives a presentation of how the coatings could function on some exposed parts of the naval powertrain. The essay investigates the possibility that the coatings can be used as a protective layer that will reduce or prevent wear on selected parts of the naval powertrains. As a basis for the essay, nanotechnology is described, as well as different reasons that wear occurs and application techniques for coatings   The conclusion is that nanostructured coatings can be applied and provide a much better result on hardness and wear resistance as of naval powertrains compared to micro-structural coatings, both for manufacturing and renovation.   The essay presents a few examples of the military utility of the nanostructure coatings as well as suggestions for further research.
Då marina enheter numera deltar i internationella missioner, kommer den nya och i många fall tuffare miljön som enheterna opererar i att påverka bland annat deras framdrivning.   Den här studien avhandlar några av de nu framtagna nanostrukturella ytbeläggningarna och ger en presentation av hur de kan fungera på några marina drivlinors utsatta delar. Studien undersöker ytbeläggningarnas möjliga förmåga att utgöra ett skyddande lager som ska minska eller i bästa fall förhindra slitaget på valda delar av marina drivlinor. Som underlag till studien beskrivs i allmänna termer nanoteknik, olika anledningar till att slitaget uppstår samt något om hur ytbeläggningen kan appliceras.   Studiens slutsats är att det med all sannolikhet går att applicera nanostrukturella ytbeläggningar och få ett mycket bättre resultat avseende hårdhet samt nötnings- och reptålighet jämfört med mikrostrukturella ytbeläggningar. Detta gäller såväl vid nytillverkning som renovering av de studerade delarna av drivlinor.   Studien ger exempel på den militära nyttan med denna ytbeläggning samt ger förslag på fortsatt forskning.
APA, Harvard, Vancouver, ISO, and other styles
40

Debbou, Mustapha. "Modélisation et commande d'un système innovant pour la propulsion navale." Thesis, Toulouse, INPT, 2014. http://www.theses.fr/2014INPT0028.

Full text
Abstract:
Les travaux menés durant cette thèse s'intéressent principalement aux avantages que peut offrir la machine asynchrone à double alimentation (MADA) dans un système de propulsion navale. Ceci est obtenu à travers les degrés de libertés additionnels qu'elle apporte, d'une part, par l'exploitation de la redondance structurelle naturelle, et d'autre part , par les stratégies de contrôle qui lui sont appliquées. La première partie de ce mémoire, présente la modélisation du propulseur innovant. Ce dernier est conçu principalement autour de la MADA comme moteur de propulsion. Il est alimenté par deux onduleurs de tension à Modulation de Largeur d'Impulsion (MLI), et entrainant une hélice à trois pales fixes et symétriques. Plusieurs stratégies de commande ont été introduites pour piloter le système. En effet, des lois de contrôle de type linéaires et non linéaires, associées à des divers modulateurs MLI ont été validées et appliquées à cette structure de propulsion. L'innovation apportée dans le cadre de ces travaux consiste à associer à l'optimisation par conception (machine et convertisseurs d'alimentation), une optimisation par la commande et ce en évaluant l'influence de ces techniques pour deux critères de dimensionnement majeurs, à savoir, les pertes dans les convertisseurs de puissances, et les bruits acoustiques et vibratoires. La propulsion navale, comme tout système embarqué, possède des exigences en matière de qualité de service non seulement en termes de performances mais aussi de fiabilité et de disponibilité. En effet, les systèmes conçus pour ce type d'application doivent assurer et garantir une continuité de service en cas d'apparition de défauts au sein des constituants du système. L'utilisation de la MADA dans les systèmes de propulsion offre une redondance structurelle naturelle et analytique, introduite par la commande, qui permet d'assurer une continuité de service du système en présence d'une défaillance dans la structure. Deux défauts sont ainsi considérés dans cette étude, un défaut de semi-conducteur de puissance dans le convertisseur de puissance et un défaut de capteur vitesse/position. Les stratégies de contrôle proposées, les modèles de propulseur établis ainsi que les reconfigurations adoptées suite aux défauts ont été validées expérimentalement sur les bancs développés au LAPLACE dans le cadre de ces travaux
This study focuses on the benefits that can be induced by the use of the Double Fed Induction Machine (DFIM) operating in motor mode for marine propulsion systems. It can be achieved by the additional degree of freedom it provides, firstly, by exploiting the natural structural redundancy, and secondly, by the alytical redundancy introduced by applied control strategies. The first part of this thesis presents the modeling of a propeller architected mainly around the DFIM and its load such as a propeller with three fixed and symmetrical blades. Several control strategies have been introduced to control the system, in fact, linear and nonlinear control laws type associated with various modulators have been validated and applied to the propulsion structure. The objective was to evaluate the influence of these techniques for two major design criteria, namely, losses in power converters, and noise and vibration noise. Naval propulsion as any embedded system has requirements for the quality of service not only in performance but also reliability and availability. Indeed, the systems designed for these types of applications must ensure and guarantee continuity of service in response to the failures in system components. The use of MADA in propulsion systems provides a natural structural and analytical redundancies which ensure system service continuity in the presence of a fault in this structure. Two faults are considered in this study, a power semiconductor fault in the power converter and a speed sensor / position failure. Control strategies proposed, the propeller modeling established and reconfigurations adopted following settings have been validated by simulation and experimentally on the real laboratory or industrial benches developed in the context of this study
APA, Harvard, Vancouver, ISO, and other styles
41

Hsu, Han-Tsung, and 許漢宗. "Propulsion Efficiency Analysis of Marine Propeller Ducted Propeller." Thesis, 1997. http://ndltd.ncl.edu.tw/handle/52564248414914139326.

Full text
Abstract:
碩士
國立中興大學
機械工程學系
85
In quest of better propulsive efficiency for ducted propeller, first we must establish genuine theoretical basis. Accordingly, in this paper we refer Lagrangian Reynolds transport equation and propulsion power analysis equationsdeveloped by Hsing-Juin Lee to derive the generalized total kinetic power ofducted propeller, the acquired kinetic power, the thrust power, the availablepropulsion power and associated propulsive efficiency. These generalizedequations involve some physical parameters including acceleration of ductedpropeller, interal flow velocity and inlet/exit pressures. Moreover, it isworthy to note that the total kinetic power is a fuction of relative elocity,not of absolute velocity. Further, we can revive the traditionally mistaken total kinetic power to own true physical meaning by redefining it as availablepropulsion power. Additionally, the traditional scheme of changing flow momentum in order to increase ducted propeller thrust will involve large energyloss in axis flow. In that light, herein we propose to diverge the duct forincreasing the outlet pressure, thus increasing the thrust of ducted propeller. Nevertheless, the genuine 3-D diffuser flow is highly complicated andoftentimes blends with secondary back flows near duct wall to form velocitydistribution as a Mexican chapeau and meanwhile increase entropy. Therefore, overly diverged duct cannot ensure upswing for thrust of ducted propeller.In the future, numerical simulation can give more precise flow status in thediverged region of ducted propeller in order to enhance the relevant propulsion analysis and design.
APA, Harvard, Vancouver, ISO, and other styles
42

Xu, Han-Zong, and 許漢宗. "Propulsion Efficiency Analysis of Marine Propeller Ducted Propeller." Thesis, 1997. http://ndltd.ncl.edu.tw/handle/64995981904447564287.

Full text
APA, Harvard, Vancouver, ISO, and other styles
43

Lan, Yuh-Jiin, and 藍玉錦. "Stress Analysis of Composite Marine Propeller." Thesis, 1993. http://ndltd.ncl.edu.tw/handle/15041677548620876893.

Full text
Abstract:
碩士
國立臺灣大學
造船工程學系
81
The stress distribution of fiber-reinforced composite marine propeller was investigated in this paper. The analysis of a marine propeller blade is rather difficult by the fact of complicated geometry of propeller. So,the mathematical transfermation of coordinate and curve fitting technique were applied to generate a 3-D solid of blade. Computer graphic was also used to show the contour of marine blade. The projected view of propeller blade was applied to make a mesh of finite element and used in the stress analysis of propeller. A conventional three-blade and a high skew seven-blade propeller were considered in the analysis. To explain the characteristics of mechanics of composite, candilever straight and curved beams were applied in the stress anslysis. From the analyzing results, it is shown that the deflection and twist angle of straight beam is dominated by the magnitude of coupled term D11 and D16. For curved beam, the deflection pattern was affected by stack sequency, fiber orientation and geometric shape. A conventional and a high skew propeller blade were chosen in the numerical analysis. Different kind of materials, isotropic and composite, were considered in the analysis for comparison. From numerical results,it is seem that the prinicipal stress contours on the pressure side and the suction side for both blade exhibit a similar trend. The mazimum stress is located near the mid-chord of blade-hub intersection. The maximum deflection occurred the tip of the blade. Aanlysis results also compared with previous paper. It shown a reasonable agreement.
APA, Harvard, Vancouver, ISO, and other styles
44

Lin, Ching-Chieh, and 林敬傑. "Study on the Optimization of FRP Marine Propeller." Thesis, 2003. http://ndltd.ncl.edu.tw/handle/77917895368523853566.

Full text
Abstract:
博士
國立臺灣大學
工程科學與海洋工程學系
91
Traditional propellers are made of high-stiffness metal material. They deform only slightly and are usually designed to work at a constant speed, operating at reduced efficiency at other speeds. This research designs a composite propeller that operates over a wider range of speeds. The deformation of propeller is determined by arranging the stacking sequence to produce propellers that are more efficient than those made of metal. Interest in the application of genetic algorithms (GA) to the stacking sequence of composite laminates has grown in recent years. However, the huge calculation time of GA is a major problem for designers. In this study, a local improvement is inserted into a standard GA, and the real calculation, by finite element analysis (FEA) for example, required in the local search is replaced by a regression model. Accordingly, the improved GA converges much sooner than a standard GA and the calculation time is greatly reduced. The regression analysis applies chosen trigonometric functions as base functions, and estimates objective function values accurately using only few sample points. The GA with local improvement is then applied to the composite propeller, and the amount of calculation is reduced by over half. In the optimization of composite propeller, the optimal stacking sequence sought by the GA does not outperform a metal propeller, and a pre-deformed design is then used to solve this problem. A smallest pitch stacking sequence is obtained using a GA first, and then the propeller is displaced in the opposite direction to form a pre-deformed propeller. The pre-deformed propeller finally meets the demands of optimization and outperforms the traditional metal propeller. Finally, an experiment is made to verify the result of calculation. The characteristics and the deformation of the propeller is found to be concord with the result of the integrated calculation in this study. The pitch of the propeller is reduced when the axial inflow velocity is reduced. The propeller outperforms traditional metal propellers.
APA, Harvard, Vancouver, ISO, and other styles
45

Hsin-Wei, Hsu. "Parametric study of marine propeller performance based on numerical simulation." 2006. http://www.cetd.com.tw/ec/thesisdetail.aspx?etdun=U0016-1303200709283893.

Full text
APA, Harvard, Vancouver, ISO, and other styles
46

Hsu, Hsin-Wei, and 許忻瑋. "Parametric study of marine propeller performance based on numerical simulation." Thesis, 2006. http://ndltd.ncl.edu.tw/handle/53192137595165840204.

Full text
Abstract:
碩士
國立清華大學
動力機械工程學系
94
The main objective of present study is to develop an automatic grid generation procedure for the parametric performance analysis of the marine propellers. The simulation platform is based on the STAR-CD software to compute the flowfield of the 2695 model propeller provided by the china ship building company. There are also open water tests data available at different advance ratios to allow careful examinations of the prediction capability of the present numerical procedure. Also, CSBC provides simulation results using panel method, which can also be used as supplementary criteria of the results. A series of parametric studies are performed on the model 2695 to explore the influences of the propeller efficiency, which include skew, rake, area ratio (chord length) and the number of the propeller blades. The results indicate that the increase of skew has little effects on the performance of the propeller. However, increase of the rake and chord length do reduce the performance of the propeller, The reduction of blade number, on the other hand, increase the efficiency, however, the thrust of force is reduced due to decrease of the blade number.
APA, Harvard, Vancouver, ISO, and other styles
47

SU, GUAN-LUN, and 蘇冠倫. "Dynamic Response of Marine Propeller Structure under Detonation External Force." Thesis, 2019. http://ndltd.ncl.edu.tw/handle/xhr4s7.

Full text
Abstract:
碩士
大葉大學
機械與自動化工程學系
107
The difference between a military ship and a general ship is that the warship needs to have the ability to fight, and the modern warship must have the ability to resist strong water knocking. The knocking has a great impact on the ship. This knock is either numerical analysis or actual explosion test. It is necessary, so how to improve the ability of military ships to maintain their combat capability after being subjected to detonation is a very important factor. When a military ship can withstand a weapon attack, even if it can withstand considerable damage to the hull, its important equipment fails. It will also make the ship lose its combat capability, so the seismic capacity is an important indicator for improving combat and survivability. In the US military MIL-STD-901D specification, the warships are based on safety factors, navigation, and the equipment is divided into Grad A, Grad B, and Grad C according to the importance of the equipment and the system is verified by physical test before loading. To ensure that Class A and Class B equipment meets the knock requirements. However, if the equipment, system, and pedestal on the ship are too bulky and heavy, they cannot use the physical test or the actual ship test to verify their detonation ability. Due to the excessive volume and weight considerations, it is impossible to test in the laboratory. The actual ship knock test is quite time-consuming and requires a lot of money. Therefore, the US Naval Laboratory developed a dynamic design analysis method-DDAM (Dynamic Design Analysis Method) to perform anti-knock analysis for equipment that cannot be subjected to actual ship knock test. In this thesis, the marine propeller structure is taken as the research object, and the ABAQUS finite element software is used as the tool to perform the seismic analysis under the external force of the propeller structure by the free vibration, forced vibration and dynamic design analysis (DDAM). The research results show that the marine propeller structure used in this paper has a natural frequency variation range of 0~23Hz, and the external vibration excitation frequency of forced vibration falls between 0~19Hz. In order to avoid resonance, the ship equipment is designed. You should refer to avoiding this vibration range to avoid sensitive frequencies in this range. The ship propeller structure is analyzed by Dynamic Design Analysis (DDAM), and there is obvious stress concentration at the joint between the blade and the tail shaft. The maximum von Mises stress is 535.3 MPa, which has exceeded the value of the stress of the manganese bronze material. Therefore, The design and material selection of the propeller needs to be studied and discussed.
APA, Harvard, Vancouver, ISO, and other styles
48

Hsu, Wen-Yen, and 許文彥. "Prediction of underwater noise from a marine propeller by acoustic analogy." Thesis, 2018. http://ndltd.ncl.edu.tw/handle/ttf3qa.

Full text
Abstract:
碩士
國立臺灣大學
工程科學及海洋工程學研究所
106
The objective of this thesis is to simulate the acoustic pressure field of a marine propeller. The flow field of a marine propeller is generated by software based on RANS. The method for calculating acoustic pressure used in this thesis is based on Ffowcs Williams-Hawking(FW-H) analogy. The partial differential and integral terms in FW-H acoustic wave equation are substituted with Finite difference method and Numerical integration. Besides, this thesis uses an inviscid flow field function generated by point source to verify the method reliability based on FW-H. When calculating the acoustic pressure of marine propeller, the relationship between sound pressure and distribution of sound source strength is investigated. The difference of sound pressure for far field and near field is discussed.
APA, Harvard, Vancouver, ISO, and other styles
49

Chen, Chao-Hung, and 陳朝宏. "Computing the radiating noise of a marine propeller by porous formulation." Thesis, 2019. http://ndltd.ncl.edu.tw/handle/paz997.

Full text
Abstract:
碩士
國立臺灣大學
工程科學及海洋工程學研究所
107
The objective of this thesis is to simulate the acoustic pressure field of a marine propeller. The unsteady flow field of a marine propeller is generated by RANS. Two methods are used for calculating acoustic pressure in this thesis, fowcs Williams-Hawkings (FW-H) analogy and Porous Formulation. The differential terms and integrals in the formulations are approximated by Finite difference and numerical integration. At beginning, this thesis uses an inviscid function generated by a point source to verify the method based on FW-H. At last, this thesis uses the method of images in the Potential theory to set up a free surface boundary condition, and uses Porous Formulation to calculate sound pressure of an underwater marine propeller.
APA, Harvard, Vancouver, ISO, and other styles
50

McIntyre, Duncan. "Predicting cavitation-induced noise from marine propellers." Thesis, 2021. http://hdl.handle.net/1828/12552.

Full text
Abstract:
Noise pollution threatens marine ecosystems, where animals rely heavily on sound for navigation and communication. The largest source of underwater noise from human activity is shipping, and propeller-induced cavitation is the dominant source of noise from ships. Mitigation strategies require accurate methods for predicting cavitation-induced noise, which remains challenging. The present thesis explores prediction and modelling strategies for cavitation-induced noise from marine propellers, and provides insight into models that can be used both during propeller design and to generate intelligent vessel control strategies. I examined three distinct approaches to predicting cavitation-induced noise, each of which is discussed in one of the three main chapters of this thesis: a high-fidelity computational fluid dynamics scheme, a parametric mapping procedure, and the use of field measurements. Each of these three chapters presents different insight into the acoustic behaviour of cavitating marine propellers, as well both real and potential strategies for mitigating this critical environmental emission. A combined experimental and numerical study of noise from a cavitating propeller, focused on both the fundamental importance of experimental findings and the effectiveness of the numerical modelling strategy used, is detailed in the first main chapter of this thesis. The experimental results highlighted that loud cavitation noise is not necessarily associated with high-power or high-speed propeller operation, affirming the need for intelligent vessel operation strategies to mitigate underwater noise pollution. Comparison of the experimental measurements and simulations revealed that the simulation strategy resulted in an over-prediction of sound levels from cavitation. Analysis of the numerical results and experiments strongly suggested that the cavitation model implemented in the simulations, a model commonly used for marine propeller simulations, was responsible for the over-prediction of sound levels. Ships are powered primarily by combustion engines, for which it is possible to generate "maps" relating the emission of pollutants to the engine’s speed and torque; the second main chapter of this thesis presents the methodology I developed for generating similar "maps" relating the level of cavitation-induced noise to the speed and torque of a ship's propeller. A proof-of-concept of the method that used the model propeller from the first main chapter is presented. To generate the maps, I used a low-order simulation technique to predict the cavitation induced by the propeller at a range of different speed and torque combinations. A pair of semi-empirical models found in the literature were combined to provide the framework for predicting noise based on cavitation patterns. The proof-of-concept map shows a clear optimal operating regime for the propeller. The final main chapter of this thesis presents an analysis of field noise measurements of coastal ferries in commercial operation, the data for which were provided by an industrial partner. The key finding was the identification of cavitation regime changes with variation in vessel speed by their acoustic signatures. The results provide a basis for remotely determining which vessels produce less noise pollution when subject to speed limits, which have been implement in critical marine habitats, and which vessels produce less noise at a specific optimum speed.
Graduate
APA, Harvard, Vancouver, ISO, and other styles
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography