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.
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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 (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 aluminu
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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 (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 fa
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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 o
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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 (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 an
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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
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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 (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.<br>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.<br>"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
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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, un
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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 ex
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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 cal
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Books on the topic "Aluminum alloys – Fatigue"

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

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

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Piascik, Robert S. Environmental fatigue of an Al-Li-Cu alloy. 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. National Aerospace Laboratory, 1994.

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Lü, Shengli. Lü he jin jie gou fu shi sun shang yan jiu yu ping jia. 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. 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. AGARD, North Atlantic Treaty Organization, 1998.

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

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

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Properties of aluminum alloys: Fatigue data and the effects of temperature, product form, and processing. 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. 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. 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. 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. 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. 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. 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. 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. 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. 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. 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 airp
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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. 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. 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. 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 duc
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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. 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 ten
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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. Defense Technical Information Center, 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. Defense Technical Information Center, 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. Defense Technical Information Center, 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. Defense Technical Information Center, 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. Defense Technical Information Center, 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. Defense Technical Information Center, 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. Defense Technical Information Center, 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, 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. Defense Technical Information Center, 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), 2001. http://dx.doi.org/10.2172/791299.

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You might also be interested in the extended bibliographies on the topic 'Aluminum alloys – Fatigue' for particular source types:
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