Bibliografie tematiche / Metal fatigue

Letteratura scientifica selezionata sul tema "Metal fatigue"

Autore: Grafiati
Pubblicato: 4 giugno 2021
Ultima modifica: 21 febbraio 2023

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Articoli di riviste sul tema "Metal fatigue"

1

Murakami, Yukitaka. "PL-2 Hydrogen-Material Interaction in Metal Fatigue". Abstracts of ATEM : International Conference on Advanced Technology in Experimental Mechanics : Asian Conference on Experimental Mechanics 2007.6 (2007): _PL—2–1_—_PL—2–8_. http://dx.doi.org/10.1299/jsmeatem.2007.6._pl-2-1_.

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Itoh, Y. Z., e H. Kashiwaya. "Low-Cycle Fatigue Properties of Steels and Their Weld Metals". Journal of Engineering Materials and Technology 111, n. 4 (1 ottobre 1989): 431–37. http://dx.doi.org/10.1115/1.3226491.

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Abstract (sommario):
Completely reversed, strain-controlled, low-cycle fatigue behavior at room temperature is investigated for steels and their weld metals. Weld metal specimens were taken from multi-pass weld metal deposited by shield metal arc welding (SMAW) and gas metal arc welding (GMAW), such that their gage length consisted entirely of the weld metal. Results indicate that there is a trend toward reduction in the low-cycle fatigue life of weld metals as compared with the base metals. In low carbon steel weld metals, the tendency described above is explained in terms of local plastic strain concentration by lack of uniformity of the multi-pass weld metals. The weld metals do not have the same mechanical properties anywhere as confirmed by hardness distribution, and the fatigue crack grows preferentially through the temper softened region in the multi-pass welds. In Type 308 stainless steel weld metals, the ductility reduction causes reductions in low-cycle fatigue life. This study leads to the conclusion that fairly accurate estimates of the low-cycle fatigue life of weld metals can be obtained using Manson’s universal slope method. However, life estimates of the Type 304 stainless steel is difficult due to a lack of ductility caused by a deformation-induced martensitic transformation.
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3

Fissolo, A., V. Maillot, G. Degallaix, S. Degallaix, N. Haddar, J. C. Le Roux, J. M. Stephan, C. Amzallag e F. Bouchet. "Multiple cracking under thermal fatigue". Revue de Métallurgie 101, n. 12 (dicembre 2004): 1087–99. http://dx.doi.org/10.1051/metal:2004112.

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4

Molent, L., e B. Dixon. "Airframe metal fatigue revisited". International Journal of Fatigue 131 (febbraio 2020): 105323. http://dx.doi.org/10.1016/j.ijfatigue.2019.105323.

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5

Shimamura, Yoshinobu, Keiichiro Tohgo, Hiroyasu Araki, Yosuke Mizuno, Shoji Kawaguchi, Masaru Hashimto e Tokuichi Inoue. "Fatigue of Metal Free Reed due to Self-Excited Oscillation". Advanced Materials Research 33-37 (marzo 2008): 267–72. http://dx.doi.org/10.4028/www.scientific.net/amr.33-37.267.

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Abstract (sommario):
Metal free reeds are used for musical instruments like harmonica. Free reeds are small, thin cantilevers, and oscillate by blowing air. It is reported that free reeds break due to fatigue during play. In order to elongate the life of free reeds, the fatigue properties should be investigated and a motion analysis method should be developed. The experimental and analytical research on metal free reed, however, has been rarely reported. In this study, two types of fatigue testing machines were developed to obtain basic fatigue characteristics. The fatigue testing machines are designed for bending fatigue of actual free reeds whose thickness is less than 400 μm. An S-N diagram is successfully obtained up to 107 cycles by using the developed fatigue testing machines. The fracture surfaces of fatigued specimens are in good agreement with those of free reeds failed in use. Then, an analytical method for the self-excited oscillation of free reeds was developed based on a mass-damper-spring model. The proposed method can take account for the shape of free reed. The self-excited oscillation of free reeds with different shape are analyzed and in good agreement with experimental results.
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6

Okazaki, M., Y. Mutoh e M. Yamaguchi. "Creep-Fatigue Fracture of Dissimilar Metal Electron Beam Welded Joints at Elevated Temperature". Journal of Engineering Materials and Technology 110, n. 3 (1 luglio 1988): 212–18. http://dx.doi.org/10.1115/1.3226039.

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Creep-fatigue tests of dissimilar-metal electron beam welded joints between A387 Gr.22 ferritic low-alloy steel and AISI 405 ferritic stainless steel were carried out under strain-controlled cycling at a temperature of 873 K. It was found that the creep-fatigue life of a dissimilar metal welded joint was significantly shorter than those of its base metals. This resulted from the strain concentration on the AISI 405 side (with the lower deformation resistance.) It was also found that the hardness distribution was one of the important measures by which the local strain distribution was reflected. Furthermore, a simple prediction method for the creep-fatigue life of dissimilar metal welded joints was proposed based on the creep-fatigue life properties of its base metals by applying the strain range partitioning approach. The predicted lives were in good agreement with the experimental results.
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Gaier, C., B. Unger e H. Dannbauer. "Multiaxial fatigue analysis of orthotropic materials". Revue de Métallurgie 107, n. 9 (ottobre 2010): 369–75. http://dx.doi.org/10.1051/metal/2011002.

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Isa, Halim, A. R. Omar, A. M. Saman, I. Othman e M. A. Ali. "Analysis of Time-to-Fatigue for Standing Jobs in Metal Stamping Industry". Advanced Materials Research 433-440 (gennaio 2012): 2155–61. http://dx.doi.org/10.4028/www.scientific.net/amr.433-440.2155.

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In metal stamping industry, almost all jobs are practically to be performed in standing position. Standing in a long period of time can lead to muscle fatigue. The objective of this study was to determine time-to-fatigue in the erector spinae, tibialis anterior, and gastrocnemius muscles of twenty production workers in a metal stamping company. The muscles activity was concurrently measured using surface electromyography (sEMG) during beginning, mid, and end of working sessions. Results of study found that gastrocnemius muscle fatigued earlier during all working sessions. In addition, working at the end of working session showed earlier fatigue than the beginning and mid of work days. The study concluded that standing in a long period of time is a cause to muscle fatigue experienced by the production workers.
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Abdulraoof Abdulrazzaq, Mohammed. "Effect of Shot Peening on Mechanical Properties for Steel AISI 1008". DJES 12, n. 2 (1 giugno 2019): 54–64. http://dx.doi.org/10.24237/djes.2019.12205.

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Residual stress has a significant effect for improving engineering properties for metals .Most of the surface treatments produce compressive residual stress at the metal surfaces, which reduce crack initiation and increasing the metal resistance to fatigue, which is shot peening process. Shot peening is usually used for this purpose for producing plastic deformations of surface of the metal which can lead to creation high residual compressive stresses at metal surface .This research include study the influence of shot peening process on fatigue resistance, surface hardness and surface roughness for low carbon steel (AISI 1008). This process accomplished with different times which were (10, 20 and 30(minutes. The result of the fatigue test showed that the fatigue limit increase when shot peening time increased and the best fatigue limit obtained when shot peening process was carried out at 30 minutes. Results of hardness test showed that surface hardness increased with increase of shot peening time. It can be seen that highest value of surface hardness is obtained from shot peening process at time (30 minutes) which is (235.1 HVN). Results of surface roughness test showed that the surface roughness of metal increased when time of shot peening increased.
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Lambert, Y., e J. Dhers. "Fatigue-corrosion des rouleaux de coulée continue". Revue de Métallurgie 87, n. 5 (maggio 1990): 491–99. http://dx.doi.org/10.1051/metal/199087050491.

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Tesi sul tema "Metal fatigue"

1

Fernandes, Paulo Jorge Luso. "Fatigue and fracture of metals in liquid-metal environments". Thesis, University of Cambridge, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.337963.

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Nowicki, Timothy. "Statistical model prediction of fatigue life for diffusion bonded Inconel 600 /". Online version of thesis, 2008. http://hdl.handle.net/1850/7984.

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Yazdanpanah, Amir. "Computer aided fatigue design". Thesis, Sheffield Hallam University, 1990. http://shura.shu.ac.uk/20587/.

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Today's competitive market requires engineers to produce reliable light weight products at low cost. This can be achieved by more effective use of computer aided engineering tools during early stages of the design process. A research programme has been undertaken to investigate the data requirements of integrating commercially available software packages (finite element analysis and fatigue life evaluation) to evaluate the integrity and durability of engineering components at the conceptual design stage. A real engineering component, in the form of a steering arm, supplied by a European truck manufacturer was used as a basis for the investigation. This is a typical vehicle component, in which, under service loading conditions, a multiaxial state of stress occurs. A geometric model of the component was created using the Prime "MEDUSA" software suite. The model was used to locate the boundary co-ordinates necessary for the development of a PAFEC Finite Element model. By imposing the conditions experienced during the service, the critical areas of the component were identified by analysing the F.E. model and a detailed description of the elastic stress/strain fields were also established. These were incorporated in an energy density approach and Neuber's uniaxial analysis to predict total local elastic/plastic strains at these critical- locations. These were compared with strain gauge measurements. The calculated results were used to plot a number of load/local strain calibration curves for the development of a load history, suitable for experimental fatigue life assessment. Fatigue crack initiation tests were performed on the steering arm using a computer controlled DARTEC multiaxial fatigue testing machine. Fatigue life assessment based on full service loading was carried out using a software package based on the critical location approach. A comparison of computerised, experimental and actual test circuit fatigue lives has been made. The work enabled a specification to be produced for the integration of the two items of software. This integrated software was developed by third parties and used to produce a computerised life map of the steering arm.
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Jethwa, Jagdish K. "The fatigue performance of adhesively-bonded metal joints". Thesis, Imperial College London, 1995. http://hdl.handle.net/10044/1/7526.

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Larsson, Tobias. "Material and fatigue properties of old metal bridges". Licentiate thesis, Luleå : Luleå University of Technology, 2006. http://epubl.ltu.se/1402-1757/2006/26/.

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Dear, Matthew Nicholas. "Fatigue in SiC fibre reinforced titanium metal matrix composites". Thesis, University of Birmingham, 2016. http://etheses.bham.ac.uk//id/eprint/6603/.

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The fatigue and interfacial characteristics of a unidirectional, SiC (SCS 6), fibre reinforced Ti 6Al 4V metal matrix composite have been investigated using a series of fatigue crack propagation, total life, and interfacial characterisation techniques. A room temperature crack arrest to catastrophic failure (CA/CF) transition was quantified using the initial stress intensity factor range ΔKapp. This transition occurred between 21 and 18 MPa√m in the three point bend geometry, and was found to be dependent on volume fraction of intact fibres bridging the crack. Increasing the test temperature to 300˚C had different effects on the resistance to fatigue crack growth depending on crack opening displacements and test piece stiffness. Total life fatigue tests revealed that the dominant failure mechanism was matrix fatigue cracking and fibre bridging. The extent of fatigue crack growth and fibre bridging was dependant on the applied stress and test temperature. The introduction of a dwell period at maximum load resulted in a small reduction in the total fatigue life. Post fatigue fibre push out tests identified that fatigue caused a reduction of interfacial properties below the as received levels. This reduction of interfacial properties was dependent on fatigue test temperature and initial loading conditions.
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Dinsley, Christopher Paul. "Fatigue properties of dissimilar metal laser welded lap joints". Thesis, Sheffield Hallam University, 2004. http://shura.shu.ac.uk/19561/.

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This work involves laser welding austenitic and duplex stainless steel to zinc-coated mild steel, more specifically 1.2mm V1437, which is a Volvo Truck Coiporation rephosphorised mild steel. The work investigates both tensile and lap shear properties of similar and dissimilar metal laser welded butt and lap joints, with the majority of the investigation concentrating on the fatigue properties of dissimilar metal laser welded lap joints. The problems encountered when laser welding zinc-coated steel are addressed and overcome with regard to dissimilar metal lap joints with stainless steel. The result being the production of a set of guidelines for laser welding stainless steel to zinc-coated mild steel. The stages of laser welded lap joint fatigue life are defined and the factors affecting dissimilar metal laser welded lap joint fatigue properties are analysed and determined; the findings suggesting that dissimilar metal lap joint fatigue properties are primarily controlled by the local stress at the internal lap face and the early crack growth rate of the material at the internal lap face. The lap joint rotation, in turn, is controlled by sheet thickness, weld width and interfacial gap. Laser welded lap joint fatigue properties are found to be independent of base material properties, allowing dissimilar metal lap joints to be produced without fatigue failure occurring preferentially in the weaker parent material, irrespective of large base material property differences. The effects of Marangoni flow on the compositions of the laser weld beads are experimentally characterised. The results providing definite proof of the stirring mechanism within the weld pool through the use of speeds maps for chromium and nickel. Keywords: Laser welding, dissimilar metal, Zinc-coated mild steel, Austenitic stainless steel, Duplex stainless steel, Fatigue, Lap joint rotation, Automotive.
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Heffern, Thomas V. "Probabilistic modeling and simulation of metal fatigue life prediction". Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://library.nps.navy.mil/uhtbin/hyperion-image/02sep%5FHeffern.pdf.

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Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, September 2002.
Thesis advisor(s): Ramesh Kolar, E. Roberts Wood. Includes bibliographical references (p. 113). Also available online.
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Marrow, Thomas James. "Fatigue mechanisms in an embrittled duplex stainless steel". Thesis, University of Cambridge, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.386998.

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Beheshti, Milad. "Fatigue life prediction of threaded pipe connection". Thesis, Brunel University, 2017. http://bura.brunel.ac.uk/handle/2438/15588.

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Abstract (sommario):
In the oil and gas industry, threaded pipe connection is frequently used to connect the casing string, drill pipe strings or production and transportation risers and pipelines. The connection is normally preloaded in order to maintain a sealed and secure connection while in service and avoid leakage. Tapered thread are a common connection and in order to introduce preload to the threaded connection when they are assembled a certain make-up torque is going to be applied. The make-up torque plus external loads result in a multiaxial stress distribution over the connection, where the threaded connections act as stress risers. Environment such as waves and currents cause dynamic loads acting on the pipe line and offshore structures. The weakest point in offshore structure is the pipe connection because of fatigue crack initiated in the connection's threads. Researchers and engineers developed a variety of patented threaded pipe connection which all claiming to improve a connection's fatigue life. The experimental data for patented designs, available in literature, is limited. Most published studies usually comprise experiments on a single connection type. For detailed fatigue analysis those published studies cannot be used since there is no uniformity in testing setup, loading conditions and damage detection technique exist. Moreover, current design curves in codes and standards lead to overly conservative or inaccurate results. The aim of this work is to provide a better understanding of the fatigue mechanisms of threaded pipe connections and to study the effect of different design features on a connection's fatigue life. The final goal is to formulate guidelines for new fatigue resistant connection designs. API connection is used as a reference in this study. Several modifications and design features are applied to the connection type. To simulate the effect of these modifications, a parametric 2D axisymmetric finite element model, ABAQUS is used. 2D finite element result are compared with a 3D model to prove its validity for both make-up. In addition, the results of the 2D axisymmetric simulation are validated by static strain gauge measurements during a make-up test and an axial tension test. The validated model is then used to evaluated the influence of the connection properties and design features on the threaded connection's behaviour. Test rigs were designed to perform axial fatigue experiment on two scales: the small-scale experiments on 1" (33.4 mm outer diameter) connections are performed in axial fatigue testing, the medium scale tests on 4.5" (114.3 mm) connections are carried out under axial tension for which a setup is developed. The majority of the performed fatigue tests are small scale experiments. Several modified configurations are tested. The S-N curve is constructed, so that the effect of certain configuration on the connection's fatigue life can be quantified. The local modification of the threaded connection's geometry as well as the connection's contact condition's contact conditions can have an important influence on the fatigue life of the connection. A beach marking technique is used to visualized the crack fronts at different moments during the tests so that exact crack shape can be seen during post-mortem analysis. The result shown that a crack initiates at the root of the last engaged thread of the male part of the connection, and propagates slowly over a large segment of the circumference, forming a long shallow crack. When the crack penetrates the pipe wall, it rapidly increases in size along two crack fronts. The shape of crack observed in beach mark analysis do not have a semi-elliptical shape as commonly used in fracture mechanics. A fatigue crack growth analysis that considers the crack as an annular flaw, is effective in describing the crack growth behaviour. The experimentally obtained S-N curves and the result from the finite element simulations are combined in multiaxial damage evolution law. The observed trend in fatigue lives of the configuration are explained by using the fatigue analysis. Using a connection's thread load distribution as a measure for its fatigue life is proven to be inaccurate. The main reason for this is that the load distribution is related to axial stresses over the connection. The fatigue life of a threaded connection is determined by the local multiaxial stress distribution and strain range around the root of the last engaged thread. These local conditions are not only the result of the load distribution, but they are also affected by the hoop stress introduced during make-up, which can additionally be affected by a changed connection stiffness. The multiaxial damage evolution law is used to analyse the influence of several features on a connection's fatigue life. It is not for all patented modifications that an increased fatigue life is predicted when applied to the API connection. The final conclusion reached is that, in order to optimize a fatigue resistant connection, several design features must be combined together. The thread shape can be optimized to obtained a low stress concentration factor and reduce the local strains at the thread root. The connection's global geometry and make-up conditions can be optimized to improve the load distribution over the threads and reduce local stresses and strains at the threads.
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Più fonti

Libri sul tema "Metal fatigue"

1

1935-, Marsh K. J., e Pook L. P, a cura di. Metal fatigue. Mineola, NY: Dover Publications, 1999.

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2

Sean, Williams. Metal fatigue. Sydney: HarperCollins, 1996.

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3

Van, Ky Dang, e Ioannis Vassileiou Papadopoulos, a cura di. High-Cycle Metal Fatigue. Vienna: Springer Vienna, 1999. http://dx.doi.org/10.1007/978-3-7091-2474-1.

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I, Stephens R., e Fuchs H. O. 1907-, a cura di. Metal fatigue in engineering. 2a ed. New York: Wiley, 2001.

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J, Comer Jess, e Handrock James L, a cura di. Fundamentals of metal fatigue analysis. Englewood Cliffs, N.J: Prentice Hall, 1990.

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Miller, K. J. Metal fatigue: Past, current and future. London: Mechanical Engineering Publications, 1991.

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Dang, Van Ky, e Papadopoulos Iōannēs V, a cura di. High-cycle metal fatique: From theory to applications. Wien: Springer, 1999.

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Alderliesten, René. Fatigue and Fracture of Fibre Metal Laminates. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-56227-8.

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D, Henry Scott, Dragolich Kathleen S, DiMatteo Nikki D e ASM International, a cura di. Fatigue data book: Light structural alloys. Materials Park, OH: ASM International, 1995.

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Tomer, Avinoam. Structure of metals through optical microscopy. [Materials Park, Ohio?]: ASM International, 1991.

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Capitoli di libri sul tema "Metal fatigue"

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Alderliesten, R. C. "Fatigue". In Fibre Metal Laminates, 155–71. Dordrecht: Springer Netherlands, 2001. http://dx.doi.org/10.1007/978-94-010-0995-9_11.

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Chawla, Nikhilesh, e Krishan K. Chawla. "Cyclic Fatigue". In Metal Matrix Composites, 227–82. New York, NY: Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4614-9548-2_8.

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Homan, J. J., R. P. G. Müller, F. Pellenkoft e J. J. M. de Rijck. "Fatigue of riveted joints". In Fibre Metal Laminates, 173–95. Dordrecht: Springer Netherlands, 2001. http://dx.doi.org/10.1007/978-94-010-0995-9_12.

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Alderliesten, René. "Acoustic Fatigue". In Fatigue and Fracture of Fibre Metal Laminates, 291–98. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-56227-8_13.

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Alderliesten, René. "Fatigue Initiation". In Fatigue and Fracture of Fibre Metal Laminates, 127–46. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-56227-8_7.

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Davoli, P. "Principles of Current Methodologies in High-Cycle Fatigue Design of Metallic Structures". In High-Cycle Metal Fatigue, 1–56. Vienna: Springer Vienna, 1999. http://dx.doi.org/10.1007/978-3-7091-2474-1_1.

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Van, K. Dang. "Introduction to Fatigue Analysis in Mechanical Design by the Multiscale Approach". In High-Cycle Metal Fatigue, 57–88. Vienna: Springer Vienna, 1999. http://dx.doi.org/10.1007/978-3-7091-2474-1_2.

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Papadopoulos, I. V. "Multiaxial Fatigue Limit Criterion of Metals". In High-Cycle Metal Fatigue, 89–143. Vienna: Springer Vienna, 1999. http://dx.doi.org/10.1007/978-3-7091-2474-1_3.

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Bignonnet, A. "Fatigue Design in Automotive Industry". In High-Cycle Metal Fatigue, 145–67. Vienna: Springer Vienna, 1999. http://dx.doi.org/10.1007/978-3-7091-2474-1_4.

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Maitournam, H. "Finite Elements Applications". In High-Cycle Metal Fatigue, 169–87. Vienna: Springer Vienna, 1999. http://dx.doi.org/10.1007/978-3-7091-2474-1_5.

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Atti di convegni sul tema "Metal fatigue"

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LOSERTOVÁ, Monika, Vojtěch KUBEŠ, Zdeněk jr ČEJKA, František FOJTÍK, Kateřina KONEČNÁ, Martin KRAUS e Tomáš ČEGAN. "Fatigue properties of Ti6Al4V prepared by selective laser melting". In METAL 2021. TANGER Ltd., 2021. http://dx.doi.org/10.37904/metal.2021.4269.

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KANDER, Ladislav, e Miroslav GREGER. "LOW-CYCLE FATIGUE OF STEEL AISI 316 AFTER ECAP". In METAL 2021. TANGER Ltd., 2021. http://dx.doi.org/10.37904/metal.2021.4123.

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ŠKODA, Jan, Monika LOSERTOVÁ, Kateřina KONEČNÁ, František FOJTÍK e Petr CZYŽ. "A STUDY OF MICROSTRUCTURE AND FATIGUE BEHAVIOUR OF A3003 ALLOY". In METAL 2021. TANGER Ltd., 2021. http://dx.doi.org/10.37904/metal.2021.4262.

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KLEJCH, Filip, e Eva SCHMIDOVÁ. "Fatigue strength degradation of thermomechanically rolled high strength steels welds". In METAL 2021. TANGER Ltd., 2021. http://dx.doi.org/10.37904/metal.2021.4141.

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HANUSOVÁ, Patrícia, Marek ROSZAK, Peter PALČEK e Milan UHRÍČIK. "Influence of Hydrogen Embrittlement on Fatigue Life of Titanium Endoprosthesis". In METAL 2021. TANGER Ltd., 2021. http://dx.doi.org/10.37904/metal.2021.4231.

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ČÍŽEK, Petr, Ladislav KANDER e Zdeněk KUBOŇ. "Effect of high - pressure hydrogen on fatigue properties of 34Crmo4 steel". In METAL 2019. TANGER Ltd., 2019. http://dx.doi.org/10.37904/metal.2019.849.

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JUDAS, Jakub, Josef ZAPLETAL e Vít JAN. "EXTREMELY LOW CYCLE FATIGUE BEHAVIOUR OF HIGH STRENGTH 2024-T351 ALUMINUM ALLOY". In METAL 2022. TANGER Ltd., 2022. http://dx.doi.org/10.37904/metal.2022.4497.

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TESAŘ, Jiří, Michal ŠVANTNER, Jiří SKÁLA, Petra HONNEROVÁ e Matyáš NOVÁK. "Thermographic method for fatigue limit determination at cyclic loading - measurement procedure overview and validation". In METAL 2019. TANGER Ltd., 2019. http://dx.doi.org/10.37904/metal.2019.709.

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ŠPIRIT, Zbyněk, Jan KAUFMAN, Josef STREJCIUS, Michal CHOCHOLOUŠEK e Josef KOTT. "Influence of Laser Shock Peening on Residual stress and Fatigue life of stainless steels". In METAL 2019. TANGER Ltd., 2019. http://dx.doi.org/10.37904/metal.2019.887.

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MORAVEC, Jaromir, Jan NOVÁK, Jiri SOBOTKA e Iva NOVÁKOVÁ. "Influence of the Welding Process on Changes in the S460MC Fine-grained Steel Joints Fatigue life". In METAL 2020. TANGER Ltd., 2020. http://dx.doi.org/10.37904/metal.2020.3501.

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Rapporti di organizzazioni sul tema "Metal fatigue"

1

Wang, Yanli, Peijun Hou e Sam Sham. Report on FY 2020 creep, fatigue and creep fatigue testing of Alloy 709 base metal at ORNL. Office of Scientific and Technical Information (OSTI), settembre 2020. http://dx.doi.org/10.2172/1671410.

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Wang, Yanli, Peijun Hou e T. Sham. Report on FY 2021 creep, fatigue and creep fatigue testing of Alloy 709 base metal at ORNL. Office of Scientific and Technical Information (OSTI), agosto 2021. http://dx.doi.org/10.2172/1813151.

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Stauffer, Amy C., e Ernest J. Czyryca. Fatigue Crack Growth Rate Behavior in Titanium Alloy Ti-5111 Weld Metal. Fort Belvoir, VA: Defense Technical Information Center, luglio 2004. http://dx.doi.org/10.21236/ada430233.

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Davidson, D. L. Micromechanisms of Fatigue Crack Growth and Fracture Toughness in Metal Matrix Composites. Fort Belvoir, VA: Defense Technical Information Center, aprile 1993. http://dx.doi.org/10.21236/ada265153.

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Wang, Yanli, e Sam Sham. Planned FY19 creep and fatigue design curve testing of Alloy 709 base metal. Office of Scientific and Technical Information (OSTI), settembre 2019. http://dx.doi.org/10.2172/1569365.

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Li, Meimei, William Soppet, Saurin Majumdar, Weiying Chen e Ken Natesan. Development of Creep-Fatigue Design Methodology for Base Metal and Weldments of G91. Office of Scientific and Technical Information (OSTI), agosto 2015. http://dx.doi.org/10.2172/1879649.

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Sun, C. T., J. F. Doyle e A. R. Leewood. Fatigue Crack Growth and Retardation Due to Overloads in Metal-Matrix Composites. Volume 2. Finite Element Analysis of Cracks in Metal Matrix Composites. Fort Belvoir, VA: Defense Technical Information Center, agosto 1986. http://dx.doi.org/10.21236/ada259445.

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Connor, Robert J., e Cem Korkmaz. Fatigue Categorization of Obliquely Oriented Welded Attachments. Purdue University, 2020. http://dx.doi.org/10.5703/1288284317210.

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Abstract (sommario):
In current bridge design specifications and evaluation manuals from the American Association of State Highway and Transportation Officials (AASHTO LRFD) (AASHTO, 2018), the detail category for base metal at the toe of transverse stiffener-to-flange fillet welds and transverse stiffener-to-web fillet welds to the direction of the web and hence, the primary stress) is Category C′. In skewed bridges or various other applications, there is sometimes a need to place the stiffener or a connection plate at an angle that is not at 90 degrees to the web. As the plate is rotated away from being 90 degrees to the web, the effective “length” of the stiffener in the longitudinal direction increases. However, AASHTO is currently silent on how to address the possible effects on fatigue performance for other angles in between these two extremes. This report summarizes an FEA study that was conducted in order to investigate and determine the fatigue category for welded attachments that are placed at angles other than 0 or 90 degrees for various stiffener geometries and thicknesses. Recommendations on how to incorporate the results into the AASHTO LRFD Bridge Design Specifications are included in this report.
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Mohanty, Subhasish, William Soppet, Saurin Majumdar e Ken Natesan. Tensile and Fatigue Testing and Material Hardening Model Development for 508 LAS Base Metal and 316 SS Similar Metal Weld under In-air and PWR Primary Loop Water Conditions. Office of Scientific and Technical Information (OSTI), settembre 2015. http://dx.doi.org/10.2172/1224989.

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Grummon, D. S., e G. Gottstein. Softening mechanisms and microstructural instabilities during high temperature, low cycle fatigue of Ni, Ni sub 3 Al and their metal matrix composites. Office of Scientific and Technical Information (OSTI), gennaio 1989. http://dx.doi.org/10.2172/5050198.

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