489 research outputs found
Fracture of aluminum naval structures
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2007."June 2007."Includes bibliographical references (leaves 238-272).Structural catastrophic failure of naval vessels due to extreme loads such as underwater or air explosion, high velocity impact (torpedoes), or hydrodynamic loads (high speed vessels) is primarily caused by fracture. Traditionally, naval structures have been designed to resist yielding, buckling and fatigue, but not fracture. Consequently, adequate methods and procedures to design ships against fracture have not been developed. The rapidly increasing application of lightweight materials, such as aluminum alloys, in the shipbuilding industry requires fundamental understanding of mechanisms and mechanics of fracture that govern naval stiffened panels. Therefore, a comprehensive tool consisting of application of advanced fracture models, material calibration, and validation through component testing is provided that will increase the survivability envelope and speed up the development process of new vessels. Cracking is a major cause of structural degradation, which is a primary source of costly repair work on metal structures. This thesis studies the structural response of various stiffened plates and compares them with unstiffened plates represented by compact tension (CT) specimens.(cont.) An extensive experimental program is presented that includes coupon testing and small and intermediate scale tests on naval aluminum structures including a variety of monolithic T-type extruded and flatbar welded specimens. Representative naval designs are selected and subjected to quasi-static loading and a number of key parameters, such as geometry, loading rate and structural configuration are evaluated with respect to fracture. Numerical modeling and analyses of ductile fracture initiation and propagation on a pre-cracked geometry using a commercial finite element code (ABAQUS), taking into account the behavior of simple uncracked material, has been performed showing a very good agreement with small and intermediate scale tests. Two major contributions of this thesis are the mapping of crack patterns in stiffened plates and the development of a methodology which enables ship designers to evaluate critical areas within a structure with respect to crack initiation, propagation, optimum material usage, and computational cost.by Konstantinos P. Galanis.Ph.D
Finite element analysis of localised rolling to reduce residual stress and distortion
Fusion welding processes cause residual stress due to the uneven heat
distribution produced by the moving welding torch. These residual stresses are
characterised by a large tensile component in the welding direction. Due to the
self-equilibrated nature of the residual stress, compressive ones are present in
the far field next to the weld seam, which can cause different kind of distortion
such as bending or buckling. Welding residual stress can be responsible of
premature failure of the components, such as stress crack corrosion, buckling,
and reduction of fatigue life. Localised rolling is a stress engineering technique
that can be used to reduce the residual stress and distortion caused by welding.
It induces plastic strain in the rolling direction, counteracting the plastic strain
produced during welding.
In this thesis three techniques were investigated, pre-weld rolling, post-weld
rolling, and in situ rolling. These techniques have been seldom studied in the
past, particularly pre-weld rolling; consequently the mechanisms are poorly
understood. Finite element models allow stress and strain development during
both welding and rolling processes to be better understood, providing an
improved understanding of the mechanisms involved and aiding process
development.
A literature survey was done to find the state of the art of the computational
welding mechanics simulations, stress management, and the residual stress
measurement techniques, as well as the knowledge gaps such as, the thermal
losses through the backing-bar in the thermal simulation, the frictional
interaction in the rolling process, and the material properties of the steel used in
the models. In the literature not many models that investigate the management
of welding residual stress were found.
After this, the general considerations and assumptions for the welding thermal
mechanical models presented in this thesis were discussed. The effect of
different backing-bar conditions, as well as different material properties where
investigated. Both influenced the residual stress profile to varying degrees. In
particular, temperature dependent heat loss to the backing-bar was necessary
to capture the improved heat loss near the weld. The distortion predicted by the
model was investigated to determine whether it was due to bending or buckling
phenomena. Lastly, the temperature distribution and residual stress predictions
were validated against thermocouple and neutron diffraction measurements
conducted by Coules et al. [1β3].
Pre-weld rolling was the first of the three rolling methods considered, in which
rolling is applied to the plates before performing GMA butt-welds. The principle
behind this technique consisted in inducing tensile residual stress in the weld
region before welding; therefore, it is similar to mechanically tensioning the
weld, which can significantly reduce the residual stress and distortion. However,
there was no significant change in the tensile residual stresses. On the other
hand, it was possible to achieve a small reduction in the distortion, when the
plates were rolled on the opposite surface to the weld; rolling in this way
induced distortion in the opposite direction to the distortion induced by welding,
reducing the magnitude of the latter. These results were compared with
experiments conducted by Coules et al. [1,4]. A subsequent investigation
combined pre-weld rolling with post-weld heating. With this additional process
the residual stress and distortion were significantly reduced, and flatter residual
stress profile was achieved.
The post-weld rolling and in situ rolling techniques were discussed afterwards.
In the post-weld rolling models, rolling was applied after the weldment was
cooled to room temperature. In in situ rolling the roller was applied on top of the
weld bead at some distance behind the torch, while it was still hot. The principle
behind these techniques consisted in applying positive plastic strain to the weld
bead region by a roller, counteracting the negative plastic strains produced in
the welding process. Two roller profiles were investigated, namely, grooved,
and double flat rollers. The post-weld rolling on top of the weld bead models,
which used the grooved roller, showed good agreement against experimental
results, producing a large reduction of the residual stress and distortion. Some
discrepancies were present when the weld toes were rolled with the dual flat
roller. The former roller was more efficient for reducing residual stress and
distortion. The influence of different friction coefficients (between the roller and
weldment, and between the backing-bar and the weldment), were investigated.
It showed significant dependency on the residual stress distribution when high
rolling loads were used. The frictional interaction constrained the contact area
inducing more compressive stress in the core of the weld bead; therefore it
produced more tensile residual stress in the surface of the weldment.
Additionally, the influence of rolling parameters on the through-thickness
residual stress variation was investigated. Low loads only influence the residual
stress near the surface, while high loads affected the material through the entire
thickness.
When the dual flat roller was used to roll next to the weld bead, significant
compressive residual stress was induce in the weld bead; however, the residual
stress reduction was very sensitive to the contact of the roller to the weld toes;
therefore, when rolling a weld bead that varies in shape along the weld, the
residual stress reduction is not uniform and varies along the length. On the
other hand, the in situ rolling did not produced significant residual stress or
distortion reduction in all the cases analysed. The rolling occurred when the
material was still hot and the residual stress was subsequently formed as the
material cooled to room temperature. Numerical modelling was a very useful
tool for understanding the development of stress and plastic strain during the
welding and rolling processes
Friction stir welding parameters influencing the fracture resistance of an Al 5083 alloy welded joint
Π€ΡΠΈΠΊΡΠΈΠΎΠ½ΠΎ Π·Π°Π²Π°ΡΠΈΠ²Π°ΡΠ΅ ΠΌΠ΅ΡΠ°ΡΠ΅ΠΌ ΠΏΡΠ΅Π΄ΡΡΠ°Π²ΡΠ° ΡΠ΅Π»Π°ΡΠΈΠ²Π½ΠΎ Π½ΠΎΠ², ΡΠ°Π²ΡΠ΅ΠΌΠ΅Π½ ΠΏΠΎΡΡΡΠΏΠ°ΠΊ Π·Π°Π²Π°ΡΠΈΠ²Π°ΡΠ° Π²Π΅Π»ΠΈΠΊΠΎΠ³ Π±ΡΠΎΡΠ° ΠΌΠ°ΡΠ΅ΡΠΈΡΠ°Π»Π°, ΠΊΠ°ΠΎ ΡΡΠΎ ΡΡ Π»Π΅Π³ΡΡΠ΅ Π°Π»ΡΠΌΠΈΠ½ΠΈΡΡΠΌΠ°, Π±Π°ΠΊΡΠ°, ΡΠΈΡΠ°Π½ΠΈΡΡΠΌΠ°, ΠΌΠ°Π³Π½Π΅Π·ΠΈΡΡΠΌΠ° ΠΈΡΠ΄. ΠΠ΅Π΄ΠΈΠ½ΡΡΠ²Π΅Π½Π° ΠΎΡΠΎΠ±ΠΈΠ½Π° ΠΎΠ²ΠΎΠ³ ΠΏΠΎΡΡΡΠΏΠΊΠ° ΡΠ΅ Π΄Π° ΡΠ΅ ΠΎΠ΄Π²ΠΈΡΠ° Ρ ΡΠ²ΡΡΡΠΎΠΌ ΡΡΠ°ΡΡ, Π±Π΅Π· ΠΏΠΎΡΠ°Π²Π΅ ΡΠΎΠΏΡΠ΅ΡΠ°. Π£ ΠΎΠ²ΠΎΡ Π΄ΠΈΡΠ΅ΡΡΠ°ΡΠΈΡΠΈ, ΠΈΡΠΏΠΈΡΠΈΠ²Π°Π½Π° ΡΠ΅ Al-Mg Π»Π΅Π³ΡΡΠ° 5083, ΠΊΠΎΡΡ ΠΎΠ΄Π»ΠΈΠΊΡΡΠ΅ Π΄ΠΎΠ±ΡΠ° ΠΊΠΎΠΌΠ±ΠΈΠ½Π°ΡΠΈΡΠ° ΡΠ²ΡΡΡΠΎΡΠ΅, ΠΆΠΈΠ»Π°Π²ΠΎΡΡΠΈ ΠΈ ΠΎΡΠΏΠΎΡΠ½ΠΎΡΡΠΈ Π½Π° ΠΊΠΎΡΠΎΠ·ΠΈΡΡ. Π’ΠΎΠΊΠΎΠΌ ΡΡΠΈΠΊΡΠΈΠΎΠ½ΠΎΠ³ Π·Π°Π²Π°ΡΠΈΠ²Π°ΡΠ° ΠΌΠ΅ΡΠ°ΡΠ΅ΠΌ, ΡΠΏΠ΅ΡΠΈΡΠ°Π»Π½ΠΎ Π΄ΠΈΠ·Π°ΡΠ½ΠΈΡΠ°Π½ Π°Π»Π°Ρ, ΠΊΠΎΡΠΈ ΡΠ΅ ΡΠΎΡΠΈΡΠ°, ΠΏΡΠΎΠ΄ΠΈΡΠ΅ Ρ ΠΌΠ°ΡΠ΅ΡΠΈΡΠ°Π», ΡΠΏΡΠ°Π²ΠΎ Ρ Π»ΠΈΠ½ΠΈΡΠΈ ΡΠΏΠ°ΡΠ°ΡΠ° Π΄Π²Π΅ ΠΏΠ»ΠΎΡΠ΅ ΠΊΠΎΡΠ΅ ΡΠ΅ Π·Π°Π²Π°ΡΡΡΡ. ΠΠ° ΠΊΠΎΠ½ΡΠ°ΠΊΡΠ½ΠΎΡ ΠΏΠΎΠ²ΡΡΠΈΠ½ΠΈ ΠΎΡΠ»ΠΎΠ±Π°ΡΠ° ΡΠ΅ ΡΠΎΠΏΠ»ΠΎΡΠ° ΠΊΠΎΡΠ° ΠΎΠΌΠ΅ΠΊΡΠ°Π²Π° ΠΌΠ°ΡΠ΅ΡΠΈΡΠ°Π», ΠΎΠ»Π°ΠΊΡΠ°Π²Π° ΠΊΡΠ΅ΡΠ°ΡΠ΅ Π°Π»Π°ΡΠ° ΡΠ· ΠΈΡΡΠΎΠ²ΡΠ΅ΠΌΠ΅Π½ΠΎ ΠΌΠ΅ΡΠ°ΡΠ΅ ΠΌΠ°ΡΠ΅ΡΠΈΡΠ°Π»Π°. ΠΠ²Π°ΠΊΠΎ Π·Π°Π²ΡΠ΅Π½ΠΈ ΡΠΏΠΎΡΠ΅Π²ΠΈ ΠΈΠΌΠ°ΡΡ ΡΠΈΡΠ°Π² Π½ΠΈΠ· ΠΏΡΠ΅Π΄Π½ΠΎΡΡΠΈ Ρ ΠΎΠ΄Π½ΠΎΡΡ Π½Π° ΠΊΠ»Π°ΡΠΈΡΠ½ΠΎ Π·Π°Π²Π°ΡΠ΅Π½Π΅ ΡΠΏΠΎΡΠ΅Π²Π΅ β ΡΠΊΡΠΏΠ½Π° ΠΏΠΎΡΡΠΎΡΡΠ° Π΅Π½Π΅ΡΠ³ΠΈΡΠ΅ Π΄Π°Π»Π΅ΠΊΠΎ ΡΠ΅ ΠΌΠ°ΡΠ°, Π½Π΅ΠΌΠ° ΠΏΠΎΡΠ°Π²Π΅ ΡΠ΅ΡΠ½ΠΈΡ
ΡΠ°Π·Π°, ΡΠ²ΡΡΡΠΎΡΠ° ΡΠΏΠΎΡΠ° ΡΠ΅ΡΡΠΎ Π±ΡΠ΄Π΅ Π²Π΅ΡΠ° Π½Π΅Π³ΠΎ ΠΊΠΎΠ΄ ΠΎΡΠ½ΠΎΠ²Π½ΠΎΠ³ ΠΌΠ°ΡΠ΅ΡΠΈΡΠ°Π»Π° ΠΈ, ΠΊΠΎΠ½Π°ΡΠ½ΠΎ, Π½Π΅ΠΌΠ° ΡΡΠ΅ΡΠ½ΠΈΡ
ΡΡΠΈΡΠ°ΡΠ° Π½Π° ΠΏΡΠΈΡΠΎΠ΄Π½Ρ ΠΎΠΊΠΎΠ»ΠΈΠ½Ρ. ΠΠΎΡΡΠΎΡΠ΅, Π½Π°ΡΠ°Π²Π½ΠΎ, ΠΈ Π½Π΅Π΄ΠΎΡΡΠ°ΡΠΈ ΠΎΠ²Π΅ ΡΠ΅Ρ
Π½ΠΎΠ»ΠΎΠ³ΠΈΡΠ΅, ΠΏΡΠ΅ ΡΠ²Π΅Π³Π° ΠΏΠΎΠ²Π΅Π·Π°Π½ΠΈ ΡΠ° Π΄ΡΠΆΠΈΠ½ΠΎΠΌ Π·Π°Π²Π°ΡΠ΅Π½ΠΈΡ
ΡΠΏΠΎΡΠ΅Π²Π° ΠΊΠΎΡΠ° Π·Π°Π²ΠΈΡΠΈ ΠΎΠ΄ Π΄ΠΈΠΌΠ΅Π½Π·ΠΈΡΠ° ΠΌΠ°ΡΠΈΠ½Π΅ Π½Π° ΠΊΠΎΡΠΎΡ ΡΠ΅ ΠΏΠΎΡΡΡΠΏΠ°ΠΊ ΠΈΠ·Π²ΠΎΠ΄ΠΈ.
Π’ΠΎΠΊΠΎΠΌ ΠΎΠ²ΠΎΠ³ ΠΏΠΎΡΡΡΠΏΠΊΠ° Π·Π°Π²Π°ΡΠΈΠ²Π°ΡΠ°, Ρ Π·ΠΎΠ½ΠΈ Π·Π°Π²Π°ΡΠ΅Π½ΠΈΡ
ΡΠΏΠΎΡΠ΅Π²Π° ΡΠ°Π²ΡΠ°ΡΡ ΡΠ΅ ΡΠ°ΡΠ½ΠΎ Π΄Π΅ΡΠΈΠ½ΠΈΡΠ°Π½Π΅ Π·ΠΎΠ½Π΅ ΡΡΠΈΡΠ°ΡΠ° ΡΠΎΠΏΠ»ΠΎΡΠ΅, ΠΊΠ°ΠΎ ΠΈ ΠΊΠΎΠ΄ ΠΏΠΎΡΡΡΠΏΠΊΠ° ΠΊΠ»Π°ΡΠΈΡΠ½ΠΎΠ³ Π·Π°Π²Π°ΡΠΈΠ²Π°ΡΠ°. ΠΠ΅ΡΡΡΠΈΠΌ, ΠΊΠΎΠ΄ ΡΡΠΈΠΊΡΠΈΠΎΠ½ΠΎΠ³ Π·Π°Π²Π°ΡΠΈΠ²Π°ΡΠ° ΠΌΠ΅ΡΠ°ΡΠ΅ΠΌ, ΠΏΠΎΡΠ°Π²ΡΡΡΠ΅ ΡΠ΅ ΠΈ Π·ΠΎΠ½Π° ΡΠ΅ΡΠΌΠΎ-ΠΌΠ΅Ρ
Π°Π½ΠΈΡΠΊΠΎΠ³ ΡΡΠΈΡΠ°ΡΠ° ΠΏΠΎΠ΄ ΡΠΈΠΌΡΠ»ΡΠ°Π½ΠΎΠ³ Π΄Π΅ΡΡΡΠ²Π° ΡΠΎΠΏΠ»ΠΎΡΠ΅ ΠΈ ΠΏΠ»Π°ΡΡΠΈΡΠ½Π΅ Π΄Π΅ΡΠΎΡΠΌΠ°ΡΠΈΡΠ΅ ΠΌΠ°ΡΠ΅ΡΠΈΡΠ°Π»Π°. Π£ ΠΎΠ²ΠΎΡ Π΄ΠΈΡΠ΅ΡΡΠ°ΡΠΈΡΠΈ, ΠΈΡΠΏΠΈΡΠΈΠ²Π°Π½ ΡΠ΅ ΡΡΠΈΡΠ°Ρ ΠΏΡΠΎΡΠ΅ΡΠ½ΠΈΡ
ΠΏΠ°ΡΠ°ΠΌΠ΅ΡΠ°ΡΠ° ΡΡΠΈΠΊΡΠΈΠΎΠ½ΠΎΠ³ Π·Π°Π²Π°ΡΠΈΠ²Π°ΡΠ° Π½Π° ΡΠ²ΡΡΡΠΎΡΡ Π·Π°Π²Π°ΡΠ΅Π½ΠΈΡ
ΡΠΏΠΎΡΠ΅Π²Π°. ΠΡΠΏΠΈΡΠΈΠ²Π°Π½ ΡΠ΅ ΡΡΠΈΡΠ°Ρ (i) ΡΠΎΡΠ°ΡΠΈΠΎΠ½Π΅ Π±ΡΠ·ΠΈΠ½Π΅ Π·Π°Π²Π°ΡΠΈΠ²Π°ΡΠ° (Ρ ΠΎΠΏΡΠ΅Π³Ρ 500 Π΄ΠΎ 800 ΠΎΠ±ΡΡΠ°ΡΠ° Ρ ΠΌΠΈΠ½ΡΡΠΈ), (ii) ΡΡΠΈΡΠ°Ρ ΡΡΠ°Π½ΡΠ»Π°ΡΠΈΠΎΠ½Π΅ Π±ΡΠ·ΠΈΠ½Π΅ (75-150 mm/min) ΠΈ, (iii) ΡΡΠΈΡΠ°Ρ Π½Π°ΠΏΠ°Π΄Π½ΠΎΠ³ ΡΠ³Π»Π° Π°Π»Π°ΡΠ° (1ΠΎ-4ΠΎ). Π‘Π²ΠΈ Π·Π°Π²Π°ΡΠ΅Π½ΠΈ ΡΠΏΠΎΡΠ΅Π²ΠΈ ΠΈΡΠΏΠΈΡΠΈΠ²Π°Π½ΠΈ ΡΡ Π½Π° ΠΎΡΠΏΠΎΡΠ½ΠΎΡΡ ΠΏΡΠ΅ΠΌΠ° ΡΠ΄Π°ΡΠ½ΠΎΡ ΠΆΠΈΠ»Π°Π²ΠΎΡΡΠΈ. ΠΡΠΌΠ΅ΡΠΈΡΠΊΠΎΠΌ ΠΎΠ±ΡΠ°Π΄ΠΎΠΌ Π΅ΠΊΡΠΏΠ΅ΡΠΈΠΌΠ΅Π½ΡΠ°Π»Π½ΠΈΡ
ΡΠ΅Π·ΡΠ»ΡΠ°ΡΠ°, ΠΎΠ΄ΡΠ΅ΡΠ΅Π½Π° ΡΠ΅ ΡΠ΄Π°ΡΠ½Π° ΠΆΠΈΠ»Π°Π²ΠΎΡΡ Π·Π°Π²Π°ΡΠ΅Π½ΠΈΡ
ΡΠΏΠΎΡΠ΅Π²Π° ΠΊΠ°ΠΎ ΠΈ Π±ΡΠ·ΠΈΠ½Π° ΠΈ Π΅Π½Π΅ΡΠ³ΠΈΡΠ° Π»ΠΎΠΌΠ°. ΠΠΎΡΠ΅Π΄ ΠΌΠ΅Ρ
Π°Π½ΠΈΡΠΊΠΈΡ
ΠΈΡΠΏΠΈΡΠΈΠ²Π°ΡΠ°, ΠΈΠ·Π²ΡΡΠ΅Π½Π° ΡΡ ΠΎΠΏΡΠ΅ΠΆΠ½Π° ΠΌΠΈΠΊΡΠΎΡΡΡΡΠΊΡΡΡΠ½Π° ΠΈΡΠΏΠΈΡΠΈΠ²Π°ΡΠ° ΠΏΡΠΈΠΌΠ΅Π½ΠΎΠΌ ΠΎΠΏΡΠΈΡΠΊΠΎΠ³ ΠΈ ΡΠΊΠ΅Π½ΠΈΠ½Π³ Π΅Π»Π΅ΠΊΡΡΠΎΠ½ΡΠΊΠΎΠ³ ΠΌΠΈΠΊΡΠΎΡΠΊΠΎΠΏΠ° (SEM). ΠΠ²Π° ΠΈΡΠΏΠΈΡΠΈΠ²Π°ΡΠ° ΠΎΠΌΠΎΠ³ΡΡΠΈΠ»Π° ΡΡ Π±ΠΎΡΠΈ ΡΠ²ΠΈΠ΄ Ρ ΠΌΠ΅Ρ
Π°Π½ΠΈΠ·Π°ΠΌ ΠΈ ΠΊΠΈΠ½Π΅ΡΠΈΠΊΡ Π΄ΡΠΊΡΠΈΠ»Π½ΠΎΠ³ Π»ΠΎΠΌΠ° Π·Π°Π²Π°ΡΠ΅Π½ΠΈΡ
ΡΠΏΠΎΡΠ΅Π²Π°...Friction stir welded is relatively new- solid-states joining process for welded several material such as aluminum, copper, titanium and magnesium. Also FSW technique is preformed in solid state without melting hence avoiding hot cracking. In this research selected aluminum 5083 alloy, it is widely used in applications in which the combination of strength and low weight is attractive. In friction stir welding (FSW) pin connected to a shoulder in rotated and slowly plunged into the joint line between two pieces of plats. When the shoulder tools rotation and contact the material surface, it generated friction heating between the welding tool and the material of the work pieces. This heat causes the latter soften without reaching the melting point and allows traversing of tool along the welding. Friction stir welding presents several benefit for joining of various alloys, specially of aluminum alloy one of the significant advantage of FSW is the heat inputs are small relative to fusion welding techniques and due to the low temperature of the process, material such as Al, Cu, Mg alloys that cannot be welded by fusion processes are easily weld by FSW. On the other hand, FSW has some drawback is often slower traverse rate then some fusion welding and exit hole left when tool is withdrawn.
Friction stir welding process generates three distinct microstructural zones that result from the welding process as following: nugget zone also known as the dynamically recrystallized zone (DRZ) where the tool piece pin passes into this zone and by experience, it has high deformation and high heat, generally consists of fine equated grains due to recrystallisation, the thermo mechanically affected zone (TMAZ) and the heat affected zone (HAZ), all zones together are called welding zone. After welded aluminum alloy tested specimens alloy by charpy impact test to evaluate absorbed energy caused the fracture material and toughness of material. Also obtained high resolution images by macro-photographs and by scanning electron microscope (SEM) to evaluate type of surface fracture and detected fracture and micro void in material then analysis material by energy dispersive x-ray spectroscopy (EDX) to shown distribution elements of chemical compound in aluminum alloy after heating and cooling precipitation. Finally, selection the optimized FSW parameters for welded aluminum 5083 alloy, it achieved higher fracture resistance in welded zone of alloy..
Latest Hydroforming Technology of Metallic Tubes and Sheets
This Special Issue and Book, βLatest Hydroforming Technology of Metallic Tubes and Sheetsβ, includes 16 papers, which cover the state of the art of forming technologies in the relevant topics in the field. The technologies and methodologies presented in these papers will be very helpful for scientists, engineers, and technicians in product development or forming technology innovation related to tube hydroforming processes
Engineering Principles
Over the last decade, there has been substantial development of welding technologies for joining advanced alloys and composites demanded by the evolving global manufacturing sector. The evolution of these welding technologies has been substantial and finds numerous applications in engineering industries. It is driven by our desire to reverse the impact of climate change and fuel consumption in several vital sectors. This book reviews the most recent developments in welding. It is organized into three sections: βPrinciples of Welding and Joining Technology,β βMicrostructural Evolution and Residual Stress,β and βApplications of Welding and Joining.β Chapters address such topics as stresses in welding, tribology, thin-film metallurgical manufacturing processes, and mechanical manufacturing processes, as well as recent advances in welding and novel applications of these technologies for joining different materials such as titanium, aluminum, and magnesium alloys, ceramics, and plastics
Thermal modelling of gas metal arc welding using finite element analysis
Thesis (M.E.Sc.) -- University of Adelaide, Dept. of Mechanical Engineering, 199
Ship collision and grounding performances
PhD ThesisThis present thesis investigates the accidental load of ship collision and grounding performances. To achieve this objective the thesis is composed of several main tasks. The main tasks comprise the rupture prediction, validation of material failure, ship grounding analysis and ship collision analysis. To predict material rupture, FLD material failure was used and validated with available experimental and FEA data. The FLD was extended to established material failure scaling laws which consider onset failure at plane strain in relation to mesh sizes. This was accomplished by running mesh convergence studies at different mesh sizes and at different FLD0. The linear material damage evolution is adopted in this case until the convergence results were satisfied. The material damage was used for all of further analysis in ship collision and grounding and employed mild steel and high tensile steel material properties. The ship grounding structure damage was investigated by deploying conical rocks at different locations of the ship's double bottom structure. The analysis focused on vertical penetration and horizontal penetration which contributed to significant damage to the structure. The ship collision analysis was investigated in various types of structures arrangement and diverse ship striking scenarios to penetrate struck ship and collide rigid wall. Furthermore, the prediction of ship collision and grounding were extended by using simplified approaches that were capable to predict ship collision to rigid wall, rigid body striking ship collided with deformable struck ship and deformable collision of striking and struck ship. Finally, this substantial amount of research work achieved the objectives of the study when the results of accidental load were validated and correlate well with experimental, empirical and FEA simulations at more than a satisfactory level
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