Relevant bibliographies by topics / Aluminum alloys – Fatigue

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Aluminum alloys – Fatigue'

Author: Grafiati
Published: 4 June 2021
Last updated: 31 January 2023

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Journal articles on the topic "Aluminum alloys – Fatigue"

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Dostál, Petr, Michal Černý, Jaroslav Lev, and David Varner. "Proportional monitoring of the acoustic emission in crypto-conditions." Acta Universitatis Agriculturae et Silviculturae Mendelianae Brunensis 59, no. 5 (2011): 31–38. http://dx.doi.org/10.11118/actaun201159050031.

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The work is aimed at studying corrosion and fatigue properties of aluminum alloys by means of acoustic emission (AE). During material degradation are acoustic events scanned and evaluated. The main objective of the article is a description of behavior of aluminum alloys degraded in specific conditions and critical degradation stages determination. The first part of the article describes controlled degradation of the material in the crypto–conditions. The acoustic emission method is used for process analyzing. This part contains the AE signals assessment and comparing aluminium alloy to steel. Then the specimens are loaded on high-cyclic loading apparatus for fatigue life monitoring. Also, the synergy of fatigue and corrosion processes is taken into account.The aim is the description of fatigue properties for aluminum alloys that have already been corrosion-degraded. Attention is also focused on the structure of fatigue cracks. The main part of the article is aimed at corrosion degradation of aluminium alloys researched in real time by means of AE. The most important benefit of AE detection/recording is that it provides information about the process in real time. Using this measurement system is possible to observe the current status of the machines/devices and to prevent serious accidents.
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Zhao, Xuehang, Haifeng Li, Tong Chen, Bao’an Cao, and Xia Li. "Mechanical Properties of Aluminum Alloys under Low-Cycle Fatigue Loading." Materials 12, no. 13 (June 27, 2019): 2064. http://dx.doi.org/10.3390/ma12132064.

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In this paper, the mechanical properties of 36 aluminum alloy specimens subjected to repeated tensile loading were tested. The failure characteristics, stress-strain hysteresis curves and its corresponding skeleton curves, stress cycle characteristics, and hysteretic energy of specimens were analyzed in detail. Furthermore, the finite element model of aluminum alloy specimens under low-cycle fatigue loading was established and compared with the experimental results. The effects of specimen parallel length, parallel diameter, and repeated loading patterns on the mechanical properties of aluminum alloys were discussed. The results show that when the specimen is monotonously stretched to fracture, the failure result from shearing break. When the specimen is repeatedly stretched to failure, the fracture of the specimen is a result of the combined action of tensile stress and plastic fatigue damage. The AA6061, AA7075, and AA6063 aluminum alloys all show cyclic softening characteristics under repeated loading. When the initial stress amplitude of repeated loading is greater than 2.5%, the repeated tensile loading has a detrimental effect on the deformability of the aluminum alloy. Finally, based on experiment research as well as the results of the numerical analysis, the calculation method for the tensile strength of aluminum alloys under low-cycle fatigue loading was proposed.
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KURUMADA, Akira, Makoto SOUMA, Takahito WATAKABE, and Goroh ITOH. "OS18F099 Effect of Hydrogen on the Fatigue Crack Propagation in Aluminum Alloys." Abstracts of ATEM : International Conference on Advanced Technology in Experimental Mechanics : Asian Conference on Experimental Mechanics 2011.10 (2011): _OS18F099——_OS18F099—. http://dx.doi.org/10.1299/jsmeatem.2011.10._os18f099-.

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BUAHOMBURA, Panya, Yukio MIYASHITA, Yoshiharu MUTOH, and NOBUSHIRO Seo. "409 Fatigue Crack Growth Behavior of FSWed Joint in Different Aluminum Alloys." Proceedings of the Materials and processing conference 2012.20 (2012): _409–1_—_409–4_. http://dx.doi.org/10.1299/jsmemp.2012.20._409-1_.

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HARLOW, D. GARY. "PARTICLE STATISTICS IN ALUMINUM ALLOYS." International Journal of Reliability, Quality and Safety Engineering 13, no. 04 (August 2006): 379–95. http://dx.doi.org/10.1142/s021853930600232x.

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Pitting corrosion and fatigue crack growth are primary degradation mechanisms that affect the durability and integrity of structures made of aluminum alloys, and they are concerns for commercial transport and military aircraft. The heterogeneous nature of aluminum alloys is the reason that these are operative damage mechanisms. Typically, there are about 2,000 constituent particles per mm2on polished surfaces. Corrosion pits commence at the constituent particles and evolve into severe pits by sustained growth through clusters of particles. The severe pits are nucleation sites for subsequent fatigue crack growth. Even when the environment is not as deleterious, fatigue cracks nucleate from clusters of particles. Thus, the role of heterogeneous clusters of constituent particles is critical to the damage evolution of aluminum alloys. To formulate stochastic models that can serve as part of structural reliability analyses for the damage evolution in aluminum alloys, it is essential that quantitative descriptions of the spatial statistics of the particles and particle clusters, including their location, size, and density are developed. The primary purpose of this effort is to estimate statistically the distribution functions of the key geometrical properties of constituent particles in aluminum alloys and their role in damage evolution.
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BIAN, Jian-Chun, Keiro TOKAJI, and Takeshi OGAWA. "Study on Fatigue Properties of Aluminum-Lithium Alloys,IV. Notch Sensitivity of Aluminum-Lithium Alloys in Fatigue." Journal of the Society of Materials Science, Japan 43, no. 490 (1994): 840–46. http://dx.doi.org/10.2472/jsms.43.840.

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Fan, Chao Hua, Yu Ting He, Heng Xi Zhang, Hong Peng Li, and Feng Li. "Predictive Model Based on Genetic Algorithm-Neural Network for Fatigue Performances of Pre-Corroded Aluminum Alloys." Key Engineering Materials 353-358 (September 2007): 1029–32. http://dx.doi.org/10.4028/www.scientific.net/kem.353-358.1029.

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In the paper, genetic algorithm is introduced in the study of network authority values of BP neural network, and a GA-NN algorithm is established. Based on this genetic algorithm-neural network method, a predictive model for fatigue performances of the pre-corroded aluminum alloys under a varied corrosion environmental spectrum was developed by means of training from the testing dada, and the fatigue performances of pre-corroded aluminum alloys can be predicted. The results indicate that genetic algorithm-neural network algorithm can be employed to predict the underlying fatigue performances of the pre-corroded aluminum alloy precisely, compared with traditional neural network.
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Wang, Xi-Shu, Xu-Dong Li, Hui-Hui Yang, Norio Kawagoishi, and Pan Pan. "Environment-induced fatigue cracking behavior of aluminum alloys and modification methods." Corrosion Reviews 33, no. 3-4 (July 1, 2015): 119–37. http://dx.doi.org/10.1515/corrrev-2014-0057.

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AbstractThis paper reviews the current corrosion fatigue strength issues of light metals, which include the corrosion fatigue cracking behaviors, such as the prior-corrosion pit deformation mechanism, the synergistic interaction between prior-corrosion pits and local stress/strain, the coupling damage behavior under mechanical fatigue loading, and the surrounding environmental factors such as a high humidity and a current 3.5 wt.% or 5.0 wt.% NaCl aqueous solution. The characterization of corrosion fatigue crack growth rate based on simple and measurable parameters (crack propagation length and applied stress amplitude or stress intensity factor) is also of great concern in engineering application. In addition, an empirical model to predict S-N curves of aluminum alloys at the environmental conditions was proposed in this paper. One of the main aims was to outline the corrosion fatigue cracking mechanism, which favors the corrosion fatigue residual life prediction of aluminum alloys subjected to the different environmental media that are often encountered in engineering services. Subsequently, this paper explores recently various surface modification technologies to enhance corrosion fatigue resistance and to improve fatigue strength. For example, the fatigue strength of 2024-T4 aluminum alloy has been modified using plasma electrolytic oxidation coating with the impregnation of epoxy resin modification method to compare with other oxide coating or uncoated substrate alloy.
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Chen, Xu, Rui Si Xing, and Xiao Peng Liu. "Multiaxial Fatigue of 6061-T6 Aluminum Alloy under Corrosive Environment." Applied Mechanics and Materials 853 (September 2016): 77–82. http://dx.doi.org/10.4028/www.scientific.net/amm.853.77.

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Aluminium alloys are widely used in the fields of automobile, machinery and naval construction. To investigate the effect of non-proportional loadings and corrosive environment on the fatigue resistance of 6061-T6 aluminum alloy, a set of uniaxial and multiaxial low cycle fatigue tests were carried out. Firstly, the results of uniaxial tests showed that the alloy exhibited cyclic hardening then cyclic softening. With the increase of stress amplitude the cyclic softening became pronounced. The increasing of plastic deformation was basically cyclically stable with small plastic strain amplitude accumulation when the stress amplitude was lower than 200MPa ,while it was increasing rapidly when the stress amplitude was higher than 220MPa. Secondly, it was observed that non-proportional cycle additional hardening of 6061-T6 aluminum alloy was little. While the fatigue life was badly affected by the loading paths. Thirdly ,the fatigue corrosion interactions were also talked about in details by performing the tests under the same loading conditions with corrosive environment. The experiment proved that the seawater corrosion has huge impact on fatigue life under pH 3. Finally, a multi-axial fatigue life prediction model was used to predict the fatigue life with or without the corrosive environment which showed a good agreement with experimental data.
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Yankin, Andrey, A. I. Mugatarov, and V. E. Wildemann. "Influence of different loading paths on the multiaxial fatigue behavior of 2024 aluminum alloy under the same amplitude values of the second invariant of the stress deviator tensor." Frattura ed Integrità Strutturale 15, no. 55 (December 28, 2020): 327–35. http://dx.doi.org/10.3221/igf-esis.55.25.

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2024 aluminum alloy is a common aeronautic material. During operations, construction elements made of aluminum alloys undertake complex cyclic loadings. Therefore, it is important to estimate the influence of these loadings on the durability of the material. Hereby, multiaxial fatigue tests with the same amplitude values of the second invariant of the stress deviator tensor are conducted, and test data are analyzed. The modified Sines method is utilized to predict fatigue experimental data. Results show that the model is accurate enough to fatigue behavior prediction of 2024 aluminum alloy.
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Dissertations / Theses on the topic "Aluminum alloys – Fatigue"

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Saoudi, Abdelhamid. "Prédiction de la rupture par fatigue dans les pièces automobiles en alliages aluminium /." Thèse, Chicoutimi : Université du Québec à Chicoutimi, 2008. http://theses.uqac.ca.

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Thèse (D.Eng.) -- Université du Québec à Chicoutimi, 2008.
La p. de t. porte en outre: Doctorat en ingénierie, thèse pour l'obtention du titre de Philosophiae Doctor en ingénierie. CaQQUQ Comprend des réf. bibliogr. (f. 174-178). Publié aussi en version électronique. CaQQUQ
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Ammar, Hany. "Effet des imperfections de la coulée sur les propriétés en fatigue des alliages de fonderie aluminium silicium = Effect of casting imperfections on the fatigue properties of aluminum-silicon casting alloys /." Thèse, Chicoutimi : Université du Québec à Chicoutimi, 2006. http://theses.uqac.ca.

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Zhao, Tianwen. "Fatigue of aluminum alloy 7075-T651 /." abstract and full text PDF (UNR users only), 2009. http://0-gateway.proquest.com.innopac.library.unr.edu/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqdiss&rft_dat=xri:pqdiss:3342620.

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Thesis (Ph. D.)--University of Nevada, Reno, 2008.
"December, 2008." Includes bibliographical references (leaves 76-83). Library also has microfilm. Ann Arbor, Mich. : ProQuest Information and Learning Company, [2009]. 1 microfilm reel ; 35 mm. Online version available on the World Wide Web.
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Jung, Hie-young. "Characterization of fatigue crack propagation in Al-Li 2090 alloys." Diss., Georgia Institute of Technology, 1994. http://hdl.handle.net/1853/20692.

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Subramaniam, Ameendraraj. "Fatigue behavior of copper zinc aluminum shape memory alloys." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk2/tape17/PQDD_0013/MQ32256.pdf.

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Wong, Yat Khin. "A phenomenological and mechanistic study of fatigue under complex loading histories." University of Western Australia. School of Mechanical Engineering, 2003. http://theses.library.uwa.edu.au/adt-WU2003.0017.

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[Truncated abstract. Please see pdf format for complete text.] Over the years much work has been done on studying sequence effects under multilevel loading. Yet, the underlying fatigue mechanisms responsible for such interactions are not fully understood. The study of fatigue under complex loading histories begins by investigating strain interaction effects arising from simple 2-step loading sequences. Fatigue for all investigations were conducted under uniaxial push-pull mode in strain-control. Fatigue is traditionally classified as either low or high cycle fatigue (LCF and HCF respectively). The boundary for LCF and HCF is not well-defined even though the fatigue life of LCF is typically dominated by crack “initiation”, while for HCF, fatigue life is usually dominated by stable crack growth. The terms LCF and HCF, apart from referring to the low and high number of fatigue cycles required for failure, also bear little physical meaning in terms of describing the state of fatigue imposed. As a result, conventional definitions of the two distinct regimes of fatigue are challenged and a new method of classifying the boundary between the two regimes of fatigue is proposed. New definitions are proposed and the terms plastically dominant fatigue (PDF) and elastically dominant fatigue (EDF) are introduced as suitable replacements for LCF and HCF respectively. PDF refers to the condition of a material undergoing significant reverse plasticity during cyclic loading, while for EDF, minimal reverse plasticity is experienced. Systematic testing of three materials, 316 L stainless steel, 6061-T6 aluminium alloy and 4340 high strength steel, was performed to fully investigate the cycle ratio trends and “damage” accumulation behaviour which resulted from a variety of loading conditions. Results from this study were carried over to investigate more complex multilevel loading sequences and possible mechanisms for interaction effects observed both under 2-step and multi-step sequences were proposed. Results showed that atypical cycle ratio trends could result from loading sequences which involve combinations of strain amplitudes from different fatigue regimes (i.e. PDF or EDF). Mean strain effects on fatigue life were also studied. The objective of this study was to identify regimes of fatigue which are significantly influenced by mean strains. Results indicated that mean strains affected EDF but not PDF. 2-step tests, similar to those performed in earlier studies were conducted to investigate the effects of mean strain on variable amplitude loading. Again, atypical cycle ratio trends were observed for loading sequences involving combinations of PDF and EDF. It is understood that fatigue crack growth interaction behaviour and mean stress effects are two dominant mechanisms which can be used to explain cycle ratio trends observed. The significance and importance of proper PDF/EDF definition and specification are also stressed. The study of fracture mechanics is an important component of any fatigue research. Fatigue crack growth in 4140 high strength steel CT specimens, under conditions of plane stress and plane strain were studied. In this investigation, the effects of R and overload ratios were also studied for both plane stress and plane strain conditions. Results indicate that differences in the point of crack “initiation” under both plane stress and plane strain conditions decrease with increasing load range, while the extent of crack retardation as a result of overloading, is greater under plane stress than plane strain conditions. The extent of crack growth retardation increases with decreasing R ratios and increasing overload ratios. The final phase of this project involves the proposal of two practical models used to predict cumulative “damage” and fatigue crack propagation in metals. The cumulative “damage” model proposed takes the form of a power law and the exponent which governs “damage” accumulation can easily be calculated by knowing the failure life, Nf, for a given strain or load level. Predictions for the “damage” model performed better when compared to other popular cumulative “damage” models. The second model proposed predicts fatigue crack growth behaviour from known monotonic and smooth specimen fatigue data. There are several benefits of having a model that can predict fatigue crack growth from monotonic and smooth specimen fatigue data: a) traditionally, engineers had to rely on expensive and time-consuming crack propagation tests to evaluate and select materials for maximum fatigue resistance, and b) monotonic and smooth specimen fatigue data are readily available. The crack propagation model is proposed to alleviate the material selection process by providing engineers a means to rapidly eliminate and narrow down selections for possible material candidates.
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Lemke, Kevin L. "A comparison of the fatigue properties of aluminum lithium 8090 forgings and 7050 aluminum plate in low strength orientations." Thesis, Georgia Institute of Technology, 1993. http://hdl.handle.net/1853/19971.

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Nelaturu, Phalgun. "Fatigue Behavior of A356 Aluminum Alloy." Thesis, University of North Texas, 2016. https://digital.library.unt.edu/ark:/67531/metadc849720/.

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Metal fatigue is a recurring problem for metallurgists and materials engineers, especially in structural applications. It has been responsible for many disastrous accidents and tragedies in history. Understanding the micro-mechanisms during cyclic deformation and combating fatigue failure has remained a grand challenge. Environmental effects, like temperature or a corrosive medium, further worsen and complicate the problem. Ultimate design against fatigue must come from a materials perspective with a fundamental understanding of the interaction of microstructural features with dislocations, under the influence of stress, temperature, and other factors. This research endeavors to contribute to the current understanding of the fatigue failure mechanisms. Cast aluminum alloys are susceptible to fatigue failure due to the presence of defects in the microstructure like casting porosities, non-metallic inclusions, non-uniform distribution of secondary phases, etc. Friction stir processing (FSP), an emerging solid state processing technique, is an effective tool to refine and homogenize the cast microstructure of an alloy. In this work, the effect of FSP on the microstructure of an A356 cast aluminum alloy, and the resulting effect on its tensile and fatigue behavior have been studied. The main focus is on crack initiation and propagation mechanisms, and how stage I and stage II cracks interact with the different microstructural features. Three unique microstructural conditions have been tested for fatigue performance at room temperature, 150 °C and 200 °C. Detailed fractography has been performed using optical microscopy, scanning electron microscopy (SEM) and electron back scattered diffraction (EBSD). These tools have also been utilized to characterize microstructural aspects like grain size, eutectic silicon particle size and distribution. Cyclic deformation at low temperatures is very sensitive to the microstructural distribution in this alloy. The findings from the room temperature fatigue tests highlight the important role played by persistent slip bands (PSBs) in fatigue crack initiation. At room temperature, cracks initiate along PSBs in the absence of other defects/stress risers, and grow transgranularly. Their propagation is retarded when they encounter grain boundaries. Another major finding is the complete transition of the mode of fatigue cracking from transgranular to intergranular, at 200 °C. This occurs when PSBs form in adjacent grains and impinge on grain boundaries, raising the stress concentration at these locations. This initiates cracks along the grain boundaries. At these temperatures, cyclic deformation is no longer microstructure- dependent. Grain boundaries don’t impede the progress of cracks, instead aid in their propagation. This work has extended the current understanding of fatigue cracking mechanisms in A356 Al alloys to elevated temperatures.
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Jordon, James Brian. "EXPERIMENTS AND MODELING OF FATIGUE AND FRACTURE OF ALUMINUM ALLOYS." MSSTATE, 2008. http://sun.library.msstate.edu/ETD-db/theses/available/etd-11062008-110529/.

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In this work, understanding the microstructural effects of monotonic and cyclic failure of wrought 7075-T651 and cast A356 aluminum alloys were examined. In particular, the structure-property relations were quantified for the plasticity/damage model and two fatigue crack models. Several types of experiments were employed to adapt an internal state variable plasticity and damage model to the wrought alloy. The damage model was originally developed for cast alloys and thus, the model was modified to account for void nucleation, growth, and coalescence for a wrought alloy. In addition, fatigue experiments were employed to determine structure-property relations for the cast alloy. Based on microstructural analysis of the fracture surfaces, modifications to the microstructurally-based MultiStage fatigue model were implemented. Additionally, experimental fatigue crack results were used to calibrate FASTRAN, a fatigue life prediction code, to small fatigue-crack-growth behavior. Lastly, a set of experiments were employed to explore the damage history effect associated with cast and wrought alloys and to provide motivation for monotonic and fatigue modeling efforts.
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Arcari, Attilio. "Enhanced strain-based fatigue methodology for high strength aluminum alloys." Diss., Virginia Tech, 2010. http://hdl.handle.net/10919/26178.

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The design of any mechanical components requires an understanding of the general statical, dynamical and environmental conditions where the components will be operating to give a satisfactory results in terms of performance and endurance. The premature failure of any components is undesirable and potentially catastrophic, therefore predictions on performances and endurances of components to proceed with repair or substitution is vital to the stability of the structure where the component is inserted. The capability of a component of withstanding fatigue loading conditions during service is called fatigue life and the designed predictions can be conservative or non conservative. Improvements to a strain based approach to fatigue were obtained in this study, studying the effects of mean stresses on fatigue life and investigating cyclic mean stress relaxation of two aluminum alloys, 7075-T6511 and 7249-T76511, used in structural aircraft applications. The two aluminum alloys were tested and their fatigue behavior characterized. The project, entirely funded by NAVAIR, Naval Air Systems Command, and jointly coordinated with TDA, Technical Data Analysis Inc., was aimed to obtain fatigue data for both aluminum alloys, with particular interest in 7249 alloy because of its enhanced corrosion resistance, and to give guidelines for improving the performances of FAMS, Fatigue Analysis of Metallic Structures, a life prediction software from the point of view of both mean stress effects and mean stress relaxation. The sensitivity of engineering materials to mean stresses is of high relevance in a strain based fatigue approach. The performance of the most common models used to calculate mean stress correction factors was studied for the two aluminum alloys 7075 and 7249 to give guidelines in the use of those for life predictions. Not only mean stresses have a high influence on fatigue life, but they are also subjected to transient cyclic behaviors. The following study considered both an empirical approach and a plasticity theory approach to simulate and include these transient effects in life calculations. Results will give valid directions to a successful modification of FAMS like any other life calculation software to include in the picture transient phenomena.
Ph. D.
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Books on the topic "Aluminum alloys – Fatigue"

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Piascik, Robert S. Environmental fatigue in aluminum-lithium alloys. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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Piascik, Robert S. Environmental fatigue of an Al-Li-Cu alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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Piascik, Robert S. Environmental fatigue of an Al-Li-Cu alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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Lameris, J. The effect of the environment on the fatigue properties of ARALL-3. Amsterdam: National Aerospace Laboratory, 1994.

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Lü, Shengli. Lü he jin jie gou fu shi sun shang yan jiu yu ping jia. Xian: Xi bei gong ye ta xue chu ban she, 2009.

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Schwarmann, L. Material data of high-strength aluminium alloys for durability evaluation of structures: Fatigue strength, crack propagation, fracture toughness. Düsseldorf: Aluminium-Verlag, 1986.

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Bucci, R. J. Aluminum alloy forgings property/performance attributes: Focus: fatigue and durability service capabilities = Les pièces forgées en alliage d'aluminium les attributs de performance/caractéristiques thèmes : fatigue et durabilité capacités en service. Neuilly-sur-Seine, France: AGARD, North Atlantic Treaty Organization, 1998.

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Zhao, W. Near-threshold fatigue crack propagation and closure behaviour in an aluminium alloy. U.K: Institution of Mechanical Engineers, 1985.

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Wanhill, R. J. H. Corrosion fatigue crack arrest in aluminium alloys: Basic data. Amsterdam: National Aerospace Laboratory, 1987.

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Properties of aluminum alloys: Fatigue data and the effects of temperature, product form, and processing. Materials Park, Ohio: ASM International, 2008.

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Book chapters on the topic "Aluminum alloys – Fatigue"

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Tiryakioǧlu, M., P. D. Eason, and J. Campbell. "Fatigue Life of Ablation Cast 6061-T6 Components." In ICAA13: 13th International Conference on Aluminum Alloys, 491–97. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch71.

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Saleema, N., P. Gauthier, and X. G. Chen. "Corrosion Fatigue Mechanism on Hot-Forged AA6082 Aluminum Alloy." In ICAA13: 13th International Conference on Aluminum Alloys, 397–403. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch59.

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Edo, Masakazu, Masatoshi Enomoto, and Yoshimasa Takayama. "Fatigue and Creep Properties of Al-Si Brazing Filler Metals." In ICAA13: 13th International Conference on Aluminum Alloys, 737–42. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch108.

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Huxhold, Stefan, Frank Balle, Guntram Wagner, and Dietmar Eifler. "Fatigue Behavior and Damage Monitoring of Ultrasonic Welded Hybrid Joints." In ICAA13: 13th International Conference on Aluminum Alloys, 505–10. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch73.

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Reynolds, Anthony P., Bob Wheeler, and Kumar V. Jata. "Deformation, Fracture and Fatigue in a Dispersion Strengthened Aluminum Alloy." In Lightweight Alloys for Aerospace Application, 87–97. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118787922.ch8.

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Mbuya, T. O., J. Crump, I. Sinclair, K. A. Soady, R. C. Thomson, and P. A. S. Reed. "Short Fatigue Crack Growth Micromechanisms in a Cast Aluminium Piston Alloy." In ICAA13: 13th International Conference on Aluminum Alloys, 485–90. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch70.

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Wolf, M., G. Wagner, and D. Eifler. "Ultrasonic Fatigue of SiC Particle Reinforced Aluminum in the VHCF-Regime." In ICAA13: 13th International Conference on Aluminum Alloys, 553–58. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch81.

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Srinivasan, Raghavan, and M. Ashraf Imam. "Role of Dispersoids on the Fatigue Behavior of Aluminum Alloys: A Review." In Fatigue of Materials III, 11–22. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-48240-8_2.

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Samuel, Ehab, Chang-Qing Zheng, Amine Bouaicha, and Mohamed Bouazara. "Fatigue Behavior in Rheocast Aluminum 357 Suspension Arms Using the SEED Process." In ICAA13: 13th International Conference on Aluminum Alloys, 151–56. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch23.

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Daniélou, A., JP Ronxin, C. Nardin, and JC Ehrström. "Fatigue Resistance of Al-Cu-Li and Comparison with 7xxx Aerospace Alloys." In ICAA13: 13th International Conference on Aluminum Alloys, 511–16. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch74.

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Conference papers on the topic "Aluminum alloys – Fatigue"

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Miscow, Guilherme Farias, Joa˜o Carlos Ribeiro Pla´cido, Paulo Emi´lio Valada˜o de Miranda, and Theodoro Antoun Netto. "Aluminum Drill Pipe Fatigue Analysis." In ASME 2004 23rd International Conference on Offshore Mechanics and Arctic Engineering. ASMEDC, 2004. http://dx.doi.org/10.1115/omae2004-51409.

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While drilling extended reach wells, the weight per foot of the drill string is a critical design parameter that can limit the depth to be reached. One practical solution is the use of drill pipes made of alternative materials to the conventional steel drill pipes. The most direct options are titanium and aluminum. Titanium is in general impaired due to its high cost, although the titanium alloy Ti-6Al4V has already been used in the airplane industry. More recently, Russia has been manufacturing drill pipes using aluminum alloys of the system Al-Cu-Mg, similar to alloys 2024, also used in airplanes. These pipes present a reasonable commercial cost. Drill pipe fatigue damage occurs under cyclic loading conditions due to, for instance, rotation in curved sections of the well. Failures caused by crack nucleation and propagation are one of the highest risks to the structural integrity of these pipes. Usually, failure mechanisms develop in the transition region of the tool joint. Several mechanical and metallurgical factors affect the fatigue life of drill pipes. The former are mainly geometric discontinuities such as transition zones, pits and slip marks. The latter are related to the size and distribution of crystalline grains, phases and second phase particles (inclusions). In this study, the roles played by both factors in the fatigue life of drill pipes are studied through an experimental test program. The fundamental fatigue mechanisms are investigated via laboratory tests in small-scale coupons performed in an opto-mechanical fatigue apparatus. Additionally, full-scale fatigue testes on three aluminum drill pipes were performed. The pipes tested are being used in the horizontal section of some extended reach wells in the Northeast of Brazil.
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Engler-Pinto, C. C., R. J. Frisch, J. V. Lasecki, J. E. Allison, X. Zhu, and J. W. Jones. "High Cycle Fatigue of Cast Aluminum Alloys at Ultrasonic Frequency." In SAE 2006 World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2006. http://dx.doi.org/10.4271/2006-01-0540.

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Dalla, P. T., I. K. Tragazikis, D. A. Exarchos, and T. E. Matikas. "The effect of corrosion on the fatigue life of aluminum alloys." In SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring, edited by Norbert G. Meyendorf, Theodoros E. Matikas, and Kara J. Peters. SPIE, 2016. http://dx.doi.org/10.1117/12.2219893.

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Yang, Jian, Wei Zhang, and Yongming Liu. "Subcycle Fatigue Crack Growth Mechanism Investigation for Aluminum Alloys and Steel." In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-1499.

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da Silva Antunes, Ana Márcia Barbosa, Carlos Antonio Reis Pereira Baptista, Miguel Justino Ribeiro Barboza, and André Luis Moreira de Carvalho. "High Cycle Fatigue Behavior of AA 6351 and AA 7050 Aluminum Alloys." In 24th SAE Brasil International Congress and Display. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2015. http://dx.doi.org/10.4271/2015-36-0296.

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Ro¨ttger, Karsten, Terry L. Jacobs, and Gerhard Wilcke. "Deep Rolling Efficiently Increases Fatigue Life." In World Tribology Congress III. ASMEDC, 2005. http://dx.doi.org/10.1115/wtc2005-63093.

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Deep rolling is a manufacturing process that efficiently increases the fatigue life of dynamically loaded components. It combines three effects to enhance fatigue strength, tribological properties and corrosion of a surface. Deep rolling: • Smoothes the surface; • Induces deep compressive stress in the surface zone; • Work-hardens the surface zone. The technology has developed into a modern, widely applicable process that improves part performance and achieves lightweight design. It has successfully been applied on stainless steels, alloy steels, brass, tool steels, nickel alloys, cast and ductile irons, aluminum, magnesium and titanium alloys [1,2,3].
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Engler-Pinto, Carlos C., John V. Lasecki, James M. Boileau, and John E. Allison. "A Comparative Investigation on the High Temperature Fatigue of Three Cast Aluminum Alloys." In SAE 2004 World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2004. http://dx.doi.org/10.4271/2004-01-1029.

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Paiva Martins, Gabriela Cristina, Carlos Filipe Cardoso Bandeira, Gabriela Wegmann Lima, and Jaime T. P. Castro. "Evaluation of the Fatigue Limits of Aluminum Alloys by Thermographic and eN techniques." In 7th International Symposium on Solid Mechanics. ABCM, 2019. http://dx.doi.org/10.26678/abcm.mecsol2019.msl19-0147.

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Obert, B., K. Ngo, J. Hashemi, S. Ekwaro-Osire, and T. P. Sivam. "Quantification of Corrosion in 7075-T6 Aluminum Alloy." In ASME 1999 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/imece1999-0622.

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Abstract In aging aircraft the synergetic interaction between corrosion and fatigue has been shown to impact the life expectancy of aluminum alloys. The objective of this study was to quantify the effects of corrosion, in terms of mass loss, on the static strength and fatigue life of 7075-T6-aluminum alloy. This was an experimental study conducted on samples with laboratory-controlled corrosion of varying mass loss levels at their mid-surface on one side. The specimens were covered with special masking material to allow corrosion only in the desired area. Both fatigue life and the ultimate tensile strength of the specimens were observed to drop significantly with small amounts of mass loss (less than 5%). After the initial decrease the UTS was observed to decrease linearly with additional mass-loss. The fatigue life of the specimens decreased significantly with additional mass loss. The topology of the pits, and the related subsurface damage hinted at existence of areas of high stress concentration resulting in the immediate reduction of UTS and fatigue life of the specimens.
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Wang, Chuangang, Yanxiang Lu, Qingqun Shan, and Guoqing Gou. "Influence of Plate Thickness on the Fatigue Properties of A7N01 Aluminum Alloys Welded Joints." In 2015 International Conference on Advanced Material Engineering. WORLD SCIENTIFIC, 2015. http://dx.doi.org/10.1142/9789814696029_0041.

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Reports on the topic "Aluminum alloys – Fatigue"

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Brockenbrough, J. R., R. J. Bucci, A. J. Hinkle, J. Liu, and P. E. Magnusen. Role of Microstructure on Fatigue Durability of Aluminum Aircraft Alloys. Fort Belvoir, VA: Defense Technical Information Center, April 1993. http://dx.doi.org/10.21236/ada265627.

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Brockenbrough, J. R., R. J. Bucci, A. J. Hinkle, J. Liu, and P. E. Magnusen. Role of Microstructure on Fatigue Durability of Aluminum Aircraft Alloys. Fort Belvoir, VA: Defense Technical Information Center, August 1993. http://dx.doi.org/10.21236/ada272116.

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Williams, J. J., and N. Chawla. Environmental Effects on Fatigue Crack Growth in High Performance Aluminum Alloys. Fort Belvoir, VA: Defense Technical Information Center, March 2009. http://dx.doi.org/10.21236/ada501490.

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Ritchie, Robert O. Fatigue Behavior of Long and Short Cracks in Wrought and Powder Aluminum Alloys. Fort Belvoir, VA: Defense Technical Information Center, November 1985. http://dx.doi.org/10.21236/ada166466.

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Koch, Gerhardus H., Elise L. Hagerdorn, and Alan P. Berens. Effect of Preexisting Corrosion on Fatigue Cracking of Aluminum Alloys 2024-T3 and 7075-T6. Fort Belvoir, VA: Defense Technical Information Center, August 1995. http://dx.doi.org/10.21236/ada430616.

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Tirpak, J. D. Constant-Load-Amplitude Fatigue Crack Growth Testing of Cast Aluminum Alloys A201-T7 and A357-T6. Fort Belvoir, VA: Defense Technical Information Center, November 1985. http://dx.doi.org/10.21236/ada163494.

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Lee, Eun U., and Henry C. Sanders. Microstructural Effect on Fatigue of 7075 Aluminum Alloy. Fort Belvoir, VA: Defense Technical Information Center, January 2002. http://dx.doi.org/10.21236/ada398914.

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Vu, Chinh. Fatigue Characteristics of New ECO Series Aluminum 7175 Alloy. Portland State University Library, January 2000. http://dx.doi.org/10.15760/etd.6861.

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Lee, E. U., R. E. Taylor, and B. Pregger. Spectrum Fatigue of 7075-T651 Aluminum Alloy under Overloading and Underloading. Fort Belvoir, VA: Defense Technical Information Center, March 2016. http://dx.doi.org/10.21236/ad1005358.

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Mark F. Horstemeyer. Microstructure-Property Relations in Fatigue of a Cast A356-T6 Aluminum Alloy. Office of Scientific and Technical Information (OSTI), August 2001. http://dx.doi.org/10.2172/791299.

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