Relevant bibliographies by topics / Nickel-base superalloys

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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 'Nickel-base superalloys'

Author: Grafiati
Published: 4 June 2021
Last updated: 7 September 2023

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Journal articles on the topic "Nickel-base superalloys"

1

Meher, Subhashish. "New Nickel-Base Superalloys Withstand Extreme Temperatures." AM&P Technical Articles 177, no. 4 (May 1, 2019): 26–28. http://dx.doi.org/10.31399/asm.amp.2019-04.p026.

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Abstract Hot section components of next-generation energy systems call for superalloys that can handle the heat. This article describes some recent advances in superalloy research and development, including characterization and modeling tools that are key to developing and understanding the formation of new superalloys capable of withstanding extreme environments.
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Jiang, Zhao Jun, Jun Wang, and Dong Mei Cao. "Research Progress in Nickel Base Single Crystal Superalloys." Key Engineering Materials 861 (September 2020): 113–21. http://dx.doi.org/10.4028/www.scientific.net/kem.861.113.

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Nickel base single crystal superalloy is widely used in hot end parts of aeroengine because of its excellent creep, fatigue and oxidation resistance. In the face of strong market demand and the emergence of new technologies and methods, in 2019, nickel-based single crystal superalloys have made remarkable achievements in preparation and heat treatment processes, repair techniques, test methods, characterization methods, theoretical simulation analysis and composition design, which continuously promotes the development of nickel base single crystal superalloy to the direction of high performance and low cost. The present work reviews the progresses from preparation and heat treatment process, repair technology of service alloy structure, service evaluation of alloy, high flux composition design. The progress in the design, preparation and engineering application of superalloy materials will eventually promote the development of a new generation of aeroengine.
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Stewart, Calvin M., and Ali P. Gordon. "Strain and Damage-Based Analytical Methods to Determine the Kachanov–Rabotnov Tertiary Creep-Damage Constants." International Journal of Damage Mechanics 21, no. 8 (December 21, 2011): 1186–201. http://dx.doi.org/10.1177/1056789511430519.

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In the power generation industry, the goal of increased gas turbine efficiency has led to increased operating temperatures and pressures necessitating nickel-base superalloy components. Under these conditions, the tertiary creep regime can become the dominant form of creep deformation. In response, the classical Kachanov–Rabotnov coupled creep-damage constitutive model is often used to predict the creep deformation and damage of Ni-base superalloys. In this model, the secondary creep behavior can be determined through analytical methods while the tertiary creep behavior is often found using trial and error or numerical optimization. Trial and error may produce no constants. Numerical optimization can be computationally expensive. In this study, a strain-based and damage-based approach to determine the tertiary creep behavior of nickel-base superalloys has been developed. Analytically determined constants are found for a given nickel-base superalloy. Creep deformation and damage evolution curves are compared. Methods to deal with stress dependence are introduced and studied.
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Monteiro, Waldemar A., and Ingrid A. Dos Santos. "Microstructural evolution of a nickel-based superalloy." Proceedings, annual meeting, Electron Microscopy Society of America 48, no. 4 (August 1990): 936–37. http://dx.doi.org/10.1017/s0424820100177817.

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Superalloys are indispensable for the superior perfomance and efficien of jet engine turbine disks,turbine blades,combustors,roket shells and many other devices and components used in various industries, in Cluding nuclear, space and aeronautics.Over the last thirty years,nickel-base superalloys has undergone more structural studies than any other superalloy as a result of attempts to correlate its properties to microstructure and heat treatment. To avoid contradictory or inconsistent findings, it is also necessary a carefully microstructural observation of the employed starting materials. In the present paper,we report morphologies relating to the as cast , forged and heat-treated Ni-base superalloy by transmission and scanning electron microscopy. This superalloy contain intermettallic compounds and carbides. The alloy in study was an as cast and also forged Ni-Fe based superalloy with the following chemical composition:
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Chen, Shao Hsien, Sen Chieh Su, Po Chun Chang, Shuo Yan Chou, and Kong King Shieh. "The Machinability of MAR-M247 Superalloy." Advanced Engineering Forum 1 (September 2011): 155–59. http://dx.doi.org/10.4028/www.scientific.net/aef.1.155.

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Nickel-base superalloy is a special super heat resistant alloy developed by U.S in 1970s. It is mainly applied to turbine parts as well as high-temperature components. Nickel-base superalloys exhibit an excellent high strength, low thermal conductivity and creep resistance as well as work hardening. It is the most difficult to be machined with high-speed cutting among different sorts of high-temperature superalloys and is a material presenting multifold challenges for machining. The purpose of this study aims at the machinability of Nickel-base alloys. Engineering statistical analysis was employed to observe the cutting speeds, feed rates and surface roughness at first place. The researcher further applied the half-normal probability plot (HNPP), Pareto analysis and ANOVA to identify the cross effects and probed into the characteristics of Nibase alloy.
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Liu, Chenguang, Huan Xu, Hui Zhang, Peiyuan Liu, Gong Yang, Lili Cui, and Haiwen Wang. "Research Progress of the Effects of Trace S Element on the Microstructure of Cast Nickel-base Superalloys." E3S Web of Conferences 299 (2021): 02004. http://dx.doi.org/10.1051/e3sconf/202129902004.

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In the process of alloy melting and vacuum pouring, the impurity S element will inevitably be introduced into the nickel-base superalloys, which will cause adverse effects on the microstructure and properties of the cast nickel-base superalloys. In this paper, the research progress of S element in cast nickel-base superalloys is summarized. The effects of S element on the microstructure are described in detail from experimental researches and first-principles. The reasons for the grain boundary embrittlement caused by S atom are discussed, and the authors wish to provide some references for the better development of cast nickel-base superalloys.
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Chapman, Neil, Simon Gray, Joy Sumner, and John Nicholls. "Surface Roughness Evolution to Identify Incubation Time for Hot Corrosion of Nickel-Base Superalloys: CMSX-4, CM247LC DS and IN6203DS at 550 °C." Oxidation of Metals 94, no. 5-6 (September 24, 2020): 447–63. http://dx.doi.org/10.1007/s11085-020-10001-y.

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AbstractIn the absence of protective scales, nickel-base superalloys have an extremely limited hot corrosion incubation period before increased rates of attack are experienced. This paper reports on the nickel-base superalloys: CMSX-4, CM247LC DS and IN6203DS subjected to 550 °C hot corrosion exposures of durations ranging from 0 to 800 h, during which none of the superalloys developed a fully protective scale. The aim of the research was to identify the incubation period of each superalloy and this was achieved by means of surface roughness evaluations. A metrology exercise was performed on the cross section of test specimens which produced Cartesian data points which were subsequently converted to Ra and Rz data. Statistical analysis of the results suggested the incubation period lasted approximately 400, 500 and 200 h, respectively, for each superalloy. It was concluded that refractory metal phases within the microstructure were associated with the relatively short IN6203DS incubation period. This paper demonstrates that monitoring the changes in surface roughness provides a plausible method to identify the transition from incubation to propagation when studying 550 °C hot corrosion attack.
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Dreshfield, Robert L. "Defects in Nickel-Base Superalloys." JOM 39, no. 7 (July 1987): 16–21. http://dx.doi.org/10.1007/bf03258034.

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Rettig, Ralf, Astrid Heckl, Steffen Neumeier, Florian Pyczak, Matthias Göken, and Robert F. Singer. "Verification of a Commercial CALPHAD Database for Re and Ru Containing Nickel-Base Superalloys." Defect and Diffusion Forum 289-292 (April 2009): 101–8. http://dx.doi.org/10.4028/www.scientific.net/ddf.289-292.101.

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The addition of rhenium and ruthenium to single crystal nickel-base superalloys improves the high-temperature properties of the alloys. In this work the applicability of the database TTNi7 (ThermoTech Ltd, UK) for developing 4th generation single crystal superalloys containing rhenium (Re) and ruthenium (Ru) was investigated. We systematically compared experimentally determined alloy properties to the predictions of ThermoCalc with the database TTNi7. The investigated properties were liquidus, solidus and ´ solvus temperature as well as incipient melting point and segregation. Calculations were based on thermodynamic principles with the assumption of either equilibrium or Scheil-Gulliver conditions, i.e. no diffusion in the solid and complete diffusion in the liquid. Furthermore the composition of the  and the  phase of a Re- and Ru-containing superalloy was measured and compared to calculations. Our results show that the database is capable of simulating general trends of 4th generation superalloys up to 6 weight percent (wt.-%) Re and 6 wt.-% Ru. The present work shows that Scheil-Gulliver calculations can only be used as a first approximation for nickel-base superalloys.
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Zhao, Hongwei. "Hydrogen embrittlement in Nickel-base superalloys Nickel-based superalloys in the petrochemical industry." Advances in Engineering Technology Research 4, no. 1 (March 18, 2023): 625. http://dx.doi.org/10.56028/aetr.4.1.625.2023.

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Due to the excellent properties of nickel-based superalloys, it is often widely used in aircraft engines, petroleum, chemical and nuclear energy. However, the use of nickel-based superalloys in petrochemical industry is usually accompanied by hydrogen embrittlement, which will lead to a decrease in its mechanical properties. Through research, it is found that reducing the generation of σ phase in nickel-based superalloys will reduce the occurrence of hydrogen embrittlement, thereby solving this problem.
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Dissertations / Theses on the topic "Nickel-base superalloys"

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Clark, A. C. "Forging of nickel-base superalloys." Thesis, Swansea University, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.636261.

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The properties of the nickel based superalloy Inconel 718 (IN 718) are insufficient for its use in the higher temperature stages at the rear of the gas turbine jet engine compressor. Considerable effort is being made to adapt the microstructure and improve the properties by thermomechanical processing, to enable the cheaper IN 718 alloy to replace the current alloy, Waspaloy, in the fabrications of these rear-end compressor disks. The initial casting of the alloy leads to an unsuitably coarse microstructure. The alloy is therefore forged in order to optimise the microstructure and hence mechanical properties. Isothermal compression tests were carried out on the alloy in the as-cast condition to investigate both dynamic and static microstructural events between 900°C and 1121°C. Strain rates ranged from 0.001s-1 to 10.0s-1 with strains from 0.1 to 0.6. Microstructural investigations revealed that complete dynamic recrystallisation was not evident in any of the samples, however partial recrystallisation occurred in samples forged at the higher temperatures and strain rates. The amount of dynamic recrystallation was found to increase primarily with temperature but also with strain rate. Complete static recrystallation was found to have occurred in tests conducted with a post-forge hold time at temperature. The degree of this recrystallisation and the resulting grain size were found to depend primarily on temperature and strain and less so on strain rate. Stress levels varied systematically with temperature and strain rates. Higher stress levels resulted from lower testing temperatures and higher strain rates. Currently property data of material in the as-cast condition is not widely available. Constitutive analysis was performed on the Stress-strain data for subsequent implementation in the forging simulation program "BILLIE". These results would then be used to provide simulations of the industrial Inco Alloys forging process.
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Zou, Xiaodong. "Impedance spectroscopy of nickel base superalloys." Thesis, Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/20307.

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Karunaratne, Mudith Sakalawalli Acharige. "Diffusional phenomena in nickel-base superalloys." Thesis, University of Cambridge, 2001. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.621097.

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Li, Ting. "Banding in nickel-base superalloys and steels." Thesis, University of British Columbia, 2007. http://hdl.handle.net/2429/344.

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Process irregularities in remelting furnace operation have an impact on the ingot solidification structure which depends on the local thermal conditions and the alloy concerned. In this work, a laboratory investigation into the structures resulting from interruptions in solid growth is presented in order to understand the cause and effect relationship between the solidification interruption and banding. The results demonstrate the range of structure, segregation and precipitation changes which are experienced by a range of alloys including Inconel 718, Nimonic 80A, Waspaloy andM50. In the case of alloys which form primary precipitates, the interruption period is shown to give rise to structure changes. Segregations are found due to the interruption. We also comment on the differences observed between industrial examples of banding and the laboratory samples which may be due to the absence of liquid movement in the latter technique. It is concluded that the interruption in solidification condition during a directionally solidification itself can produce banding through its effects on the morphology of precipitates.
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Reynolds, Gary James. "Damage rate approaches for nickel-base superalloys." Thesis, Georgia Institute of Technology, 1998. http://hdl.handle.net/1853/18863.

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Allan, Christine Dianne. "Plasticity of nickel base single crystal superalloys." Thesis, Massachusetts Institute of Technology, 1995. http://hdl.handle.net/1721.1/11771.

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Miller, Mark. "Fatigue life prediction of nickel base superalloys." Thesis, University of Southampton, 2007. https://eprints.soton.ac.uk/68693/.

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Neural networks have been used extensively in material science with varying success. It has been demonstrated that they can be very effective at predicting mechanical properties such as yield strength and ultimate tensile strength. These networks require large amounts of input data in order to learn the correct data trends. A neural network modelling process has been developed which includes data collection methodology and subsequent filtering techniques in conjunction with training of a neural network model. It has been shown that by using certain techniques to ‘improve’ the input data a network will not only fit seen and unseen Ultimate Tensile Strength (UTS) and Yield Strength (YS) data but correctly predict trends consistent with metallurgical understanding. Using the methods developed with the UTS and YS models, a Low Cycle Fatigue (LCF) life model has been developed with promising initial results. Crack initiation at high temperatures has been studied in CMSX4 in both air and vacuum environments, to elucidate the effect of oxidation on the notch fatigue initiation process. In air, crack initiation occurred at sub-surface interdendritic pores in all cases. The sub-surface crack grows initially under vacuum conditions, before breaking out to the top surface. Lifetime is then dependent on initiating pore size and distance from the notch root surface. In vacuum conditions, crack initiation has been observed more consistently from surface or close-to-surface pores - indicating that surface oxidation is in-filling/”healing” surface pores or providing significant local stress transfer to shift initiation to sub-surface pores. Complementary work has been carried out using PWA 1484 and Rene N5. Extensive data has been collected on initiating pores for all 3 alloys. A model has been developed to predict fatigue life based upon geometrical information from the initiating pores. A Paris law approach is used in conjunction with long crack propagation data. The model shows a good fit with experimental data and further improvements have been recommended in order to increase the capability of the model.
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Lambert, David. "Fatigue damage accumulation in nickel base superalloys." Thesis, University of Sheffield, 1994. http://etheses.whiterose.ac.uk/15129/.

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Tangentially oriented Waspaloy specimens taken from the bore section of a turbine disc were subjected to low cycle fatigue in the form of cyclic four point bend tests. Substantial differences in grain size and structure occurred across the section of the disc. Fatigue damage occurred primarily as a result of persistent slip band formation, cell formation, Orowan looping and precipitate shearing. A small number of grains exhibited dislocation cells, normally associated with higher stacking fault energy materials. The number and width of persistent slip bands increased with the number of cycles, but varied both between grains and stress levels. It is proposed that initially looped precipitates were subsequently sheared. Crack initiation was observed as early as 1/12 of fatigue lifetime, predominantly from inclusions. A stage-I/stage-II crack propagation transition occurred at approximate 4Kl values of 30MPa.m1/ 2 , when the plastic zone size was comparable to the material grain size. Results imply that short crack growth requires prior slip band formation.
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Arnold, K. "High temperature oxidation behaviour of nickel-base superalloys." Thesis, University of Liverpool, 2017. http://livrepository.liverpool.ac.uk/3005778/.

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The Ni-base superalloys are a popular range of materials for study following consolidation by additive manufacturing (AM) techniques, such as selective laser melting (SLM). However, very little work has been done to assess the high temperature oxidation behaviour of Ni-base superalloys fabricated by SLM, despite the fact that this class of alloy is designed primarily for operation at temperatures >650°C. In the present work, the isothermal oxidation behaviour of the Ni-base superalloys Alloy 718 and Alloy 625 was studied following consolidation by SLM. A third Ni-base superalloy, Haynes 230, which is doped with a small amount of the reactive element La, was also studied following SLM-consolidation. The same three alloys were studied in wrought form for comparison purposes. Also studied following consolidation by SLM were oxide dispersion strengthened (ODS) derivatives of Alloy 625 and Haynes 230, which contained a 0.5 Wt. % addition of Y2O3, added by mechanical alloying (MA), and developed during the project for which the present work was conducted. Comparators for the ODS variants of Alloy 625 and Haynes 230 were fabricated by spark plasma sintering (SPS). All of the alloys were oxidised in laboratory air at 900°C and the oxidation kinetics determined using thermogravimetric analysis (TGA), or from scale thickness measurements. The work has shown that SLM-consolidated Alloy 718 oxidised slightly faster than wrought Alloy 718. SLM-consolidated Haynes 230 oxidised ~3x faster than wrought Haynes 230 alloy, but SLM-consolidated Alloy 625 oxidised ~2x slower than wrought Alloy 625. The ODS variant of Alloy 625, in SLM-consolidated and SPS-consolidated forms, oxidised ~10x more slowly than wrought Alloy 625. The SLM-consolidated ODS variant of Haynes 230 oxidised at approximately the same rate as wrought Haynes 230, but in SPS-consolidated form the ODS variant of Haynes 230 oxidised ~10x faster than wrought Haynes 230. The improvement in the oxidation resistance of the ODS variant of Alloy 625 is attributed to the well-known reactive element effect, which occurs when alloys are appropriately doped with reactive elements. The reduction in the oxidation resistance of the SPS-consolidated ODS variant of Haynes 230 is attributed to overdoping of the alloy with reactive elements, which is known to decrease the oxidation resistance of nickel-base alloys. It is proposed that SLM-consolidation improves the oxidation resistance of the ODS variant of Haynes 230 by ‘slagging off’ reactive elements from the alloy during consolidation, but for the same reason, the oxidation resistance of Haynes 230 is reduced by SLM-consolidation.
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Marchand, Norman J. "Thermal-mechanical fatigue behavior of nickel-base superalloys." Thesis, Massachusetts Institute of Technology, 1986. http://hdl.handle.net/1721.1/31003.

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Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Materials Science and Engineering, 1986.
MICROFICHE COPY AVAILABLE IN ARCHIVES AND SCIENCE
Bibliography: leaves 185-199.
by Norman J. Marchand.
Sc.D.
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Books on the topic "Nickel-base superalloys"

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Patel, Shailesh Jayantilal. Advanced melting systems for nickel base superalloys. Birmingham: University of Birmingham, 1995.

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Gayda, John. Quench crack behavior of nickel-base disk superalloys. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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Painter, R. E. The quality and properties of recycled nickel base superalloys. Birmingham: University of Birmingham, 1988.

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United States. National Aeronautics and Space Administration., ed. Anisotropic constitutive modeling for nickel-base single crystal superalloys. [Cincinnati, Ohio]: University of Cincinnati, 1988.

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Berkovits, Avraham. Modelling fatigue damage accumulation in nickel base superalloys: Final report. Haifa: Technion-Israel Institute of Technology, Faculty of Aerospace Engineering, 1992.

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P, Gabb T., Miner R. V, and United States. National Aeronautics and Space Administration., eds. Fatique crack propagation of nickel-base superalloys at 650 C. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

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P, Gabb Timothy, Miner R. V, and United States. National Aeronautics and Space Administration., eds. Fatique crack propagation of nickel-base superalloys at 650 ̊C. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

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V, Nathal Michael, and United States. National Aeronautics and Space Administration., eds. Microstructure-property relationships in directionally solidified single crystal nickel-base superalloys. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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V, Nathal Michael, and United States. National Aeronautics and Space Administration., eds. Microstructure-property relationships in directionally solidified single crystal nickel-base superalloys. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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P, Gabb Timothy, and NASA Glenn Research Center, eds. The tensile properties of advanced nickel-base disk superalloys during quenching heat treatments. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Book chapters on the topic "Nickel-base superalloys"

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Zenk, C. H., S. Neumeier, M. Kolb, N. Volz, S. G. Fries, O. Dolotko, I. Povstugar, D. Raabe, and M. Göken. "The Role of the Base Element in γ′ Strengthened Cobalt/Nickel-Base Superalloys." In Superalloys 2016, 969–80. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2016. http://dx.doi.org/10.1002/9781119075646.ch103.

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Brückner, Udo, Alexander Epishin, Thomas Link, Bernard Fedelich, and Pedro D. Portella. "Dendritic Stresses in Nickel-Base Superalloys." In Materials Science Forum, 497–502. Stafa: Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-969-5.497.

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Turner, T. J., P. A. Shade, J. Schuren, M. A. Groeber, M. Miller, and M. D. Uchic. "Two Integrated Experimental and Modeling Approaches to Study Strain Distributions in Nickel and Nickel-Base Superalloy Polycrystals." In Superalloys 2012, 643–52. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118516430.ch72.

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Gu, Y. F., T. Osada, T. Yokokawa, H. Harada, J. Fujioka, D. Nagahama, and M. Okuno. "Development of Nickel-Cobalt Base P/M Superalloys for Disk Applications." In Superalloys 2016, 209–16. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2016. http://dx.doi.org/10.1002/9781119075646.ch23.

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Hasebe, Yusaku, Koichi Takasawa, Takuya Ohkawa, Eiji Maeda, and Takashi Hatano. "Grain Boundary Precipitation Strengthening of Phosphorus-Added Nickel-Iron Base Superalloy." In Superalloys 2016, 65–73. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2016. http://dx.doi.org/10.1002/9781119075646.ch7.

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Messé, O. M. D. M., and C. M. F. Rae. "Dislocations Nucleation and Interaction with Grain Boundaries in a Polycrystalline Nickel Base Superalloy." In Superalloys 2016, 831–40. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2016. http://dx.doi.org/10.1002/9781119075646.ch89.

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McLean, M. "Nickel-base superalloys: current status and potential." In High-temperature Structural Materials, 1–15. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0589-7_1.

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Mughrabi, Haël, and Ulrich Tetzlaff. "Microstructural Modifications and High-Temperature Strength of Monocrystalline Nickel-Base Superalloys." In Intermetallics and Superalloys, 108–14. Weinheim, FRG: Wiley-VCH Verlag GmbH & Co. KGaA, 2006. http://dx.doi.org/10.1002/3527607285.ch19.

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Biermann, Horst, Hua Feng, and Haël Mughrabi. "FE-Simulation of the Initial Stages of Rafting in Nickel-Base Superalloys." In Intermetallics and Superalloys, 28–33. Weinheim, FRG: Wiley-VCH Verlag GmbH & Co. KGaA, 2006. http://dx.doi.org/10.1002/3527607285.ch5.

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Yang, Yuansheng, Qingsheng Zhang, and Zhuangqi Hu. "Precipitation of Gamma Prime Phase of Nickel-Base Superalloy in Electric Field." In Intermetallics and Superalloys, 34–40. Weinheim, FRG: Wiley-VCH Verlag GmbH & Co. KGaA, 2006. http://dx.doi.org/10.1002/3527607285.ch6.

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Conference papers on the topic "Nickel-base superalloys"

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Beckman, J. P., and D. A. Woodford. "Intergranular Sulfur Attack in Nickel and Nickel-Base Alloys." In Superalloys. TMS, 1988. http://dx.doi.org/10.7449/1988/superalloys_1988_795_804.

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Shah, D. M., S. Vega, S. Woodard, and A. D. Cetel. "Primary Creep in Nickel-Base Superalloys." In Superalloys. TMS, 2004. http://dx.doi.org/10.7449/2004/superalloys_2004_197_206.

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Yoshiba, M., and O. Miyagawa. "High Temperature Corrosion Fatigue and Grain Size Control in Nickel-Base and Nickel-Iron-Base Superalloys." In Superalloys. TMS, 1988. http://dx.doi.org/10.7449/1988/superalloys_1988_825_834.

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Cetel, A. D., and D. N. Duhl. "Second Generation Columnar Grain Nickel-Base Superalloy." In Superalloys. TMS, 1992. http://dx.doi.org/10.7449/1992/superalloys_1992_287_296.

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Cetel, A. D., and D. N. Duhl. "Second-Generation Nickel-Base Single Crystal Superalloy." In Superalloys. TMS, 1988. http://dx.doi.org/10.7449/1988/superalloys_1988_235_244.

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Huron, E. S. "Serrated Yielding in a Nickel-Base Superalloy." In Superalloys. TMS, 1992. http://dx.doi.org/10.7449/1992/superalloys_1992_675_684.

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Sponseller, D. L. "Differential Thermal Analysis of Nickel-Base Superalloys." In Superalloys. TMS, 1996. http://dx.doi.org/10.7449/1996/superalloys_1996_259_270.

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Cao, W. D., and R. L. Kennedy. "Phosphorus-Boron Interaction in Nickel-Base Superalloys." In Superalloys. TMS, 1996. http://dx.doi.org/10.7449/1996/superalloys_1996_589_597.

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Lin, D., T. L. Lin, S. Huang, and C. Sun. "A Hafnium-Free Directionally Solidified Nickel-Base Superalloy." In Superalloys. TMS, 1988. http://dx.doi.org/10.7449/1988/superalloys_1988_345_354.

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Burgel, R., P. D. Portella, and J. Preuhs. "Recrystallization in Single Crystals of Nickel Base Superalloys." In Superalloys. TMS, 2000. http://dx.doi.org/10.7449/2000/superalloys_2000_229_238.

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Reports on the topic "Nickel-base superalloys"

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Anderson, I. M., M. K. Miller, L. M. Pike, and D. L. Klarstrom. Advanced microcharacterization of nickel-base superalloys. Office of Scientific and Technical Information (OSTI), February 2000. http://dx.doi.org/10.2172/752981.

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McKamey, C. G., E. P. George, C. T. Liu, J. A. Horton, C. A. Carmichael, R. L. Kennedy, and W. D. Cao. Manufacturing of nickel-base superalloys with improved high-temperature performance. Office of Scientific and Technical Information (OSTI), January 2000. http://dx.doi.org/10.2172/750965.

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Vitek, J. M., S. A. David, R. W. Reed, M. A. Burke, and T. J. Fitzgerald. Welding and Weldability of Directionally Solidified Single Crystal Nickel-Base Superalloys. Office of Scientific and Technical Information (OSTI), September 1997. http://dx.doi.org/10.2172/770471.

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Tien, John K. Understanding the HIP (Hot Isostatic Pressing) Consolidation of P/M Nickel-Base Superalloys. Fort Belvoir, VA: Defense Technical Information Center, November 1987. http://dx.doi.org/10.21236/ada187640.

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Antolovich, Stephen D. The Effect of Microstructure on the Fatigue Crack Growth Resistance of Nickel Base Superalloys. Fort Belvoir, VA: Defense Technical Information Center, December 1987. http://dx.doi.org/10.21236/ada189526.

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Milligan, Walter, Paul Sanders, Calvin White, Ninad Mohale, and John Shingledecker. Development of a Physically-Based Creep Model Incorporating Eta Phase Evolution for Nickel Base Superalloys. Office of Scientific and Technical Information (OSTI), May 2021. http://dx.doi.org/10.2172/1782793.

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Sinha, V., and J. M. Larsen. Vacuum Levels Needed to Simulate Internal Fatigue Crack Growth in Titanium Alloys and Nickel-base Superalloys: Thermodynamic Considerations. Fort Belvoir, VA: Defense Technical Information Center, March 2012. http://dx.doi.org/10.21236/ada559012.

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Gerhardt, Rosario A. Resistivity-Microstructure Relationships in Nickel Base Superalloys Used in Gas Turbine Engines for Power Generation and as Interconnects in Solid Oxide Fuel Cells. Office of Scientific and Technical Information (OSTI), February 2012. http://dx.doi.org/10.2172/1167045.

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Srinivasan, V. Life Prediction of Turbine Blade Nickel Base Superalloy Single Crystals. Fort Belvoir, VA: Defense Technical Information Center, August 1986. http://dx.doi.org/10.21236/ada172025.

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Babu, S. S., S. A. David, J. M. Vitek, and M. K. Miller. Atom probe field-ion microscopy investigation of nickel base superalloy welds. Office of Scientific and Technical Information (OSTI), November 1998. http://dx.doi.org/10.2172/290932.

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