Relevant bibliographies by topics / High cycle fatigue

Contents

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

Academic literature on the topic 'High cycle fatigue'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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Journal articles on the topic "High cycle fatigue"

1

Matikas, T. E. "A high-cycle fatigue apparatus at 20 kHz for low-cycle fatigue/high-cycle fatigue interaction testing." Fatigue & Fracture of Engineering Materials & Structures 24, no. 10 (2001): 687–97. http://dx.doi.org/10.1046/j.1460-2695.2001.00427.x.

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He, Chao, Yong Jie Liu, and Qing Yuan Wang. "Very High Cycle Fatigue Properties of Welded Joints under High Frequency Loading." Advanced Materials Research 647 (January 2013): 817–21. http://dx.doi.org/10.4028/www.scientific.net/amr.647.817.

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Very high cycle fatigue (VHCF) properties of welded joints under ultrasonic fatigue loading have been investigated for titanium alloy (TI-6Al-4V) and bridge steel (Q345). Ultrasonic fatigue tests of base metal and welded joints were carried out in ambient air at room temperature at a stress ratio R=-1. It was observed that the fatigue strength of welded joints reduced by 50-60% as compared to the base metal. The S-N fatigue curves in the range of 107~109 cycles of base metal and welded joints for both materials exhibited the characteristic of continually decreasing type. The fatigue failure st
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SHI, Jin-yuan, Yong WANG, Wang-fan LI, Zhi-cheng DENG, and Yu Yang. "ICOPE-15-C035 Crack Propagation Life under Low Cycle Fatigue and High Cycle Fatigue of Nuclear Steam Turbine Rotors." Proceedings of the International Conference on Power Engineering (ICOPE) 2015.12 (2015): _ICOPE—15——_ICOPE—15—. http://dx.doi.org/10.1299/jsmeicope.2015.12._icope-15-_131.

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Šulák, Ivo, Karel Obrtlík, and Ladislav Čelko. "High Temperature Low Cycle Fatigue Characteristics of Grit Blasted Polycrystalline Ni-Base Superalloy." Key Engineering Materials 665 (September 2015): 73–76. http://dx.doi.org/10.4028/www.scientific.net/kem.665.73.

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The present work is focused on the study of low cycle fatigue behavior of grit blasted nickel-base superalloy Inconel 713LC (IN 713LC). Grit blasting parameters are obtained. Button end specimens of IN 713LC in as-received condition and with grit blasted surface were fatigued under strain control with constant total strain amplitude in symmetrical cycle at 900 °C in air. Hardening/softening curves, cyclic stress-strain curve and fatigue life data of both materials were obtained. Both materials exhibit the same stress-strain response. It has not been observed any improvement or reduction of low
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Zhang, Wei Chang, Ming Liang Zhu, and Fu Zhen Xuan. "Experimental Characterization of Competition of Surface and Internal Damage in Very High Cycle Fatigue Regime." Key Engineering Materials 754 (September 2017): 79–82. http://dx.doi.org/10.4028/www.scientific.net/kem.754.79.

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Axially push-pull cyclic tests of a low strength rotor steel were performed up to the very high cycle fatigue regime at ambient environment under ultrasonic frequency. Fatigue tests were interrupted at selected number of cycles for surface morphology observation and roughness measurement with the help of a 3D surface measurement system (Alicona InfiniteFocusSL). The fatigue extrusions and slip band developed on the specimen surface were recorded. The influence of stress level on the number and morphology of slip band was discussed. The surface roughness of fatigue specimens was found to be inc
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Abdel Wahab, Magd, Irfan Hilmy, and Reza Hojjati-Talemi. "On the Use of Low and High Cycle Fatigue Damage Models." Key Engineering Materials 569-570 (July 2013): 1029–35. http://dx.doi.org/10.4028/www.scientific.net/kem.569-570.1029.

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In this paper, Continuum Damage Mechanics (CDM) theory is applied to low cycle and high cycle fatigue problems. Damage evolution laws are derived from thermodynamic principles and the fatigue number of cycles to crack initiation is expressed in terms of the range of applied stresses, triaxiality function and material constants termed as damage parameters. Low cycle fatigue damage evolution law is applied to adhesively bonded single lap joint. Damage parameters as function of stress are extracted from the fatigue tests and the damage model. High cycle fatigue damage model is applied to fretting
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Heinz, Stefan, and Dietmar Eifler. "Very High Cycle Fatigue and Damage Behavior of Ti6Al4V." Key Engineering Materials 664 (September 2015): 71–80. http://dx.doi.org/10.4028/www.scientific.net/kem.664.71.

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High frequency fatigue tests were carried out with a 20 kHz ultrasonic testing facility to investigate the cyclic deformation behavior of Ti6Al4V in the Very High Cycle Fatigue (VHCF) regime in detail. The S,Nf -curve at the stress ratio R = -1 shows a significant decrease of the stress amplitude and a change from surface to subsurface failures in the VHCF regime for more than 107 cycles. Microscopic investigations of the distribution of the α-and β-phase of Ti6Al4V indicate that inhomogeneities in the phase distribution are reasons for the internal crack initiation. Scanning electron microsco
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Li, Xin. "A new stress-based multiaxial high- cycle fatigue damage criterion." Functional materials 25, no. 2 (2018): 406–12. http://dx.doi.org/10.15407/fm25.02.406.

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Drobne, Matej, Peter Göncz, and Srečko Glodež. "High Cycle Fatigue Parameters of High Chromium Steel." Key Engineering Materials 488-489 (September 2011): 299–302. http://dx.doi.org/10.4028/www.scientific.net/kem.488-489.299.

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The determination of monotonic mechanical properties and high cycle fatigue parameters of high chromium steel (HCS) is presented. The monotonic mechanical properties (ultimate compressive and ultimate tensile strength) are determined using standardized testing procedures according to DIN 50125 standard. The high cycle fatigue parameters are determined using uniaxial fatigue test where the tests specimens are loaded with pure pulsating compression load (load ratio R=0 in compression) at different load levels. Therefore, a typical S-N curve and appropriate fatigue parameters (fatigue strength co
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Calabrese, Angelo Savio, Tommaso D’Antino, Pierluigi Colombi, and Carlo Poggi. "Low- and High-Cycle Fatigue Behavior of FRCM Composites." Materials 14, no. 18 (2021): 5412. http://dx.doi.org/10.3390/ma14185412.

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This paper describes methods, procedures, and results of cyclic loading tensile tests of a PBO FRCM composite. The main objective of the research is the evaluation of the effect of low- and high-cycle fatigue on the composite tensile properties, namely the tensile strength, ultimate tensile strain, and slope of the stress–strain curve. To this end, low- and high-cycle fatigue tests and post-fatigue tests were performed to study the composite behavior when subjected to cyclic loading and after being subjected to a different number of cycles. The results showed that the mean stress and amplitude
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Dissertations / Theses on the topic "High cycle fatigue"

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Knipling, Keith Edward. "High-cycle fatigue / low-cycle fatigue interactions in Ti-6Al-4V." Thesis, Virginia Tech, 2002. http://hdl.handle.net/10919/41290.

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The largest single cause of failure in fan and compressor components in the cold frontal sections of commercial and military gas turbine engines has been attributed to high cycle fatigue (HCF). Additionally, both high-cycle fatigue (HCF) and lowcycle fatigue (LCF) loadings are widely recognized as unavoidable during operation of these components and because the classic Linear Damage Rule (LDR) neglects to account for the synergistic interaction between these damage contributors, dangerous over predictions of lifetime can result. Combined low-cycle fatigue / high-cycle fatigue (HCF/LCF) loadi
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Kazymyrovych, Vitaliy. "Very high cycle fatigue of high performance steels." Licentiate thesis, Karlstad University, Faculty of Technology and Science, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:kau:diva-3066.

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<p>Many engineering components reach a finite fatigue life well above 10<sup>9 </sup>load cycles. Some examples of such components are found in airplanes, automobiles or high speed trains. For some materials the fatigue failures have lately been found to occur well after 10<sup>7</sup> load cycles, namely in the Very High Cycle Fatigue (VHCF) range. This finding contradicted the established concept of fatigue limit for these materials, which postulates that having sustained 10<sup>7</sup> load cycles the material is capable of enduring an infinite number of cycles provided that the service con
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Kazymyrovych, Vitaliy. "Very high cycle fatigue of tool steels." Doctoral thesis, Karlstads universitet, Avdelningen för maskin- och materialteknik, 2010. http://urn.kb.se/resolve?urn=urn:nbn:se:kau:diva-5877.

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An increasing number of engineering components are expected to have fatigue life in the range of 107 - 1010 load cycles. Some examples of such components are found in airplanes, automobiles and high speed trains. For many materials fatigue failures have lately been reported to occur well after 107 load cycles, namely in the Very High Cycle Fatigue (VHCF) range. This finding contradicts the established concept of a fatigue limit, which postulates that having sustained around 107 load cycles the material is capable of enduring an infinite number of cycles provided that the service conditions are
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Berchem, Klaus Herbert Hans. "High cycle fatigue and corrosion fatigue performance of two car body steels." Thesis, Imperial College London, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.414711.

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Barry, Nathan. "Lead-free solders for high-reliability applications : high-cycle fatigue studies." Thesis, University of Birmingham, 2008. http://etheses.bham.ac.uk//id/eprint/198/.

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The use of lead (Pb) in solders for electronic connections is now extensively restricted in Europe, with its use likely to be phased out completely in the medium term. Although Pb-free solders have been the subject of much research, little investigation has been carried out into their reliability for applications exposed to vibration in service. Aerospace applications, which have service lives measured in decades, are of particular pertinence. The present work shows the development and validation of a method for testing small, model solder joints in high-cycle fatigue. The tests are conducted
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Hall, Rodney H. F. "Crack growth under combined high and low cycle fatigue." Thesis, University of Portsmouth, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.290404.

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Suresh, Shyam. "Topology Optimization for Additive Manufacturing Involving High-Cycle Fatigue." Licentiate thesis, Linköpings universitet, Mekanik och hållfasthetslära, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-165503.

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Additive Manufacturing (AM) is gaining popularity in aerospace and automotive industries. This is a versatile manufacturing process, where highly complex structures are fabricated and together with topology optimization, a powerful design tool, it shares the property of providing a very large freedom in geometrical form. The main focus of this work is to introduce new developments of Topology Optimization (TO) for metal AM. The thesis consists of two parts. The first part introduces background and theory, where TO and adjoint sensitivity analysis are described. Furthermore, methodology used to
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Morrissey, Ryan J. "Frequency and mean stress effects in high cycle fatigue of Ti-6A1-4V." Thesis, Georgia Institute of Technology, 1997. http://hdl.handle.net/1853/17095.

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Pirouznia, Pouyan. "High cycle fatigue properties of stainless martensitic chromium steel springs." Thesis, KTH, Materialteknologi, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-103201.

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For many materials and components like in high speed trains and airplanes fatigue failures occur in the range of over 107 load cycles which is called the high cycle fatigue range. A modern version of the springs was invented which are applied in a certain application. Ultrasonic fatigue testing (20 kHz machine) was conducted for evaluating the steel of the springs. This research explores the fundamental understanding of high cycle fatigue testing of strip steel and assesses a stainless martensitic chromium steel at the high cycle fatigue range. Finite element modeling was conducted to gain kno
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Bantounas, Ioannis. "Microtexture and high cycle fatigue cracking in Ti-6A1-4V." Thesis, Imperial College London, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.501436.

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Books on the topic "High cycle fatigue"

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

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Dang, Van Ky, and Papadopoulos Iōannēs V, eds. High-cycle metal fatique: From theory to applications. Springer, 1999.

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Herda, D. A. A comparison of high cycle fatigue methodologies. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1992.

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Hall, Rodney H. F. Crack growth under combined high and low cycle fatigue. Portsmouth Polytechnic, School of Systems Engineering, 1991.

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A, Miller Robert, and Lewis Research Center, eds. Investigation of thermal high cycle and low cycle fatigue mechanisms of thick thermal barrier coatings. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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A, Miller Robert, and Lewis Research Center, eds. Investigation of thermal high cycle and low cycle fatigue mechanisms of thick thermal barrier coatings. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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Taghani, Nourberdi. Crack growth in gas turbine alloys due to high cycle fatigue. Portsmouth Polytechnic, Dept. of Mechanical Engineering, 1989.

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Kolenda, Janusz. Analytical procedures of high-cycle fatigue assessment of structural steel elements. Technical University of Gdańsk, 1997.

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United States. National Aeronautics and Space Administration., ed. Estimation of high temperature low cycle fatigue on the basis of inelastic strain and strainrate. For sale by the National Technical Information Service, 1986.

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Berkovits, Avraham. Estimation of high temperature low cycle fatigue on the basis of inelastic strain and strainrate. For sale by the National Technical Information Service, 1986.

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Book chapters on the topic "High cycle fatigue"

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Sander, Manuela. "Very high cycle fatigue." In Sicherheit und Betriebsfestigkeit von Maschinen und Anlagen. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-54443-3_4.

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Zimmermann, Martina. "Very High Cycle Fatigue." In Handbook of Mechanics of Materials. Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-6855-3_43-1.

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Zimmermann, Martina. "Very High Cycle Fatigue." In Handbook of Mechanics of Materials. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-10-6884-3_43.

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Milella, Pietro Paolo. "Very High Cycle Fatigue." In Fatigue and Corrosion in Metals. Springer International Publishing, 2024. http://dx.doi.org/10.1007/978-3-031-51350-3_9.

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Wang, Qingyuan, and Chao He. "Very High Cycle Fatigue." In Fatigue of Materials and Structures. CRC Press, 2025. https://doi.org/10.1201/9781003405122-6.

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Davoli, P. "Principles of Current Methodologies in High-Cycle Fatigue Design of Metallic Structures." In High-Cycle Metal Fatigue. 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. 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. 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. 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. Springer Vienna, 1999. http://dx.doi.org/10.1007/978-3-7091-2474-1_5.

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Conference papers on the topic "High cycle fatigue"

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Dang, Khanh, Rik Meininger, Joseph Gibson, Henry Wiersma, Kenneth Kim, and Michael Szedlmayer. "High Cycle Fatigue Assessment of a Diesel Engine Turbocharger." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12882.

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Many technical papers describe turbocharger turbine/compressor failures caused by foreign object damage, contaminated lube oil, lack of lubrication, high exhaust temperatures, low cycle fatigue, or overspeed. However, High Cycle Fatigue (HCF) is a potential failure mode that has not been widely assessed. This paper describes steps to investigate an HCF fatigue failure of a turbine blade. Metallurgical analysis determined that the failure surfaces are indicative of fatigue and that the initiation location coincided with the location of maximum stress as identified by finite element modal analys
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Apetre, Nicole, Attilio Arcari, Subhasis Sarkar, Nagaraja Iyyer, Nam Phan, and Peter Kang. "Fatigue Reliability Analysis for High Cycle Fatigue Regime." In 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
20th AIAA/ASME/AHS Adaptive Structures Conference
14th AIAA. American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-1385.

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Holycross, Casey M., M. H. Herman Shen, Onome E. Scott-Emuakpor, and Tommy J. George. "Energy-Based Fatigue Life Prediction for Combined Low Cycle and High Cycle Fatigue." In ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-95785.

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Gas turbine engine components are subjected to both low and high cycle fatigue as a result of mechanical and vibrational loading. Mechanical loading is generally within the low cycle fatigue regime and attributed to throttle up/throttle down cycles of various flight maneuvers or engine start-up/shut-down cycles over the course of a component’s lifetime. Vibrational loading causes high cycle fatigue of a multiaxial stress state, and is attributed to various forced and free vibration sources manifested as high order bending or torsion modes. Understanding the interaction of these two fatigue reg
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Celli, Dino, Luke Sheridan, Tommy George, Justin Warner, and Lucas Smith. "Forecasting High Cycle and Very High Cycle Fatigue Through Enhanced Strain-Energy Based Fatigue Life Prediction." In ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2024. http://dx.doi.org/10.1115/gt2024-129455.

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Abstract This study applies a novel strain-energy based fatigue life prediction method to low cycle fatigue (LCF) data of conventionally wrought and additive manufactured (AM) Inconel 718 round dog-bones, specifically focusing on cycles to failure less than 105. The objective is to forecast high cycle fatigue (HCF, 106–107) and very high cycle fatigue (VHCF &amp;gt; 107), aiming to approximate stress versus cycles to failure (SN) behavior and the inherent variability in the fatigue life of the material system. This tool is motivated by the need to characterize an expanding and diverse array of
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Jiang, L., C. R. Brooks, P. K. Liaw, and D. L. Klarstrom. "High-Cycle Fatigue of ULTIMET Alloy." In Superalloys. TMS, 2000. http://dx.doi.org/10.7449/2000/superalloys_2000_583_591.

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Ritchie, R. O. "Small Cracks and High-Cycle Fatigue." In ASME 1996 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/imece1996-0641.

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Abstract The problem of high-cycle fatigue (HCF) failures that has recently plagued the aircraft jet-engine industry is associated with the rapid growth of small defects under the action of high-frequency vibrational or resonant loading; such defects have been associated with regions of microstructural damage attributed to such processes as foreign object damage, surface fretting and low-cycle fatigue. Since the size of these defects is generally below characteristic inspection limits, traditional design and life-prediction procedures do not specifically address this problem. Moreover, from a
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El-Sayed, Mohamed E. M. "Transition From Low Cycle to High Cycle in Uniaxial Fatigue." In ASME 2013 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/imece2013-66202.

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Fatigue is the most critical failure mode of many mechanical component. Therefore, fatigue life assessment under fluctuating loads during component development is essential. The most important requirement for any fatigue life assessment is knowledge of the relationships between stresses, strains, and fatigue life for the material under consideration. These relationships, for any given material, are mostly unique and dependent on its fatigue behavior. Since the work of Wöhler in the 1850’s, the uniaxial stress versus cycles to fatigue failure, which is known as the S-N curve, is typically utili
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Métais, T. P., G. Stevens, G. Blatman, J. C. Le Roux, and R. L. Tregoning. "EDF/NRC High-Cycle Fatigue Database Proposal." In ASME 2015 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/pvp2015-45146.

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Revised fatigue curves for austenitic stainless steels are currently being considered by several organizations in various countries, including Japan, South Korea, and France. The data available from laboratory tests indicate that the mean air curve considering all available austenitic material fatigue data may be overly conservative compared to a mean curve constructed from only those data representative of a particular type of material. In other words, developing separate fatigue curves for each of the different types of austenitic materials may prove useful in terms of removing excess conser
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Blondet, Eric, and Claude Faidy. "High Cycle Thermal Fatigue in French PWR." In 10th International Conference on Nuclear Engineering. ASMEDC, 2002. http://dx.doi.org/10.1115/icone10-22762.

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Different fatigue-related incidents which occurred in the world on the auxiliary lines of the reactor coolant system (SIS, RHR, CVC) have led EDF to search solutions in order to avoid or to limit consequences of thermodynamic phenomenal (Farley-Tihange, free convection loop and stratification, independent thermal cycling). Studies are performed on mock-up and compared with instrumentation on nuclear power stations. At the present time, studies allow EDF to carry out pipe modifications and to prepare specifications and recommendations for next generation of nuclear power plants. In 1998, a new
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MA, Xuejiao, Yongneng LU, Jun WEN, and Lei XU. "High Cycle Fatigue Behavior of High Strength Steel Q960." In 2020 3rd International Conference on Electron Device and Mechanical Engineering (ICEDME). IEEE, 2020. http://dx.doi.org/10.1109/icedme50972.2020.00054.

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Reports on the topic "High cycle fatigue"

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Davidson, David L. Damage Mechanisms in High Cycle Fatigue. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada359744.

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Gallagher, J. P., R. H. van Stone, R. E. deLaneuville, P. Gravett, and R. S. Bellows. Improved High-Cycle Fatigue (HCF) Life Prediction. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada408467.

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Shockey, Donald A., Takao Kobayashi, Naoki Saito, Jean-Marie Aubry, and Alberto Grunbaum. Fractographic Analysis of High-Cycle Fatigue in Aircraft Engines. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada386670.

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Wagner, Travis, and Denise Yin. Development of Subscale Tester for High-Cycle Fatigue Evaluation. DEVCOM Army Research Laboratory, 2022. http://dx.doi.org/10.21236/ad1157677.

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Bartsch, Thomas M. High Cycle Fatigue (HCF) Science and Technology Program, 2001 Annual Report. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada408071.

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Feng, Jinwei, Ricardo Burdisso, Wing Ng, and Ted Rappaport. Turbine Engine Control Using MEMS for Reduction of High Cycle Fatigue. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada387429.

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Lin, T. H. Development of a Micromechanic Theory of Crack Initiation Under High-Cycle Fatigue. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada368833.

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Troiano, E., J. H. Underwood, D. Crayon, and R. T. Abbott. Low Cycle Notched Fatigue Behavior and Life Predictions of A723 High Strength Steels. Defense Technical Information Center, 1995. http://dx.doi.org/10.21236/ada299469.

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Rogers, Lynn, I. R. Searle, R. Ikegami, R. W. Gordon, and D. Conley. Durability Patch: Application of Passive Damping to High Cycle Fatigue Cracking on Aircraft. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada468821.

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Zha, Ge-Chenga, Ming-Ta Yang, and Fariba Fahroo. High Cycle Fatigue Prediction for Mistuned Bladed Disks with Fully Coupled Fluid-Structural Interaction. Defense Technical Information Center, 2006. http://dx.doi.org/10.21236/ada452028.

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