Relevant bibliographies by topics / Haynes

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Academic literature on the topic 'Haynes'

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Published: 4 June 2021
Last updated: 20 February 2023

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Journal articles on the topic "Haynes"

1

Haynes, John. "John Haynes." Wasafiri 21, no. 1 (March 2006): 22–23. http://dx.doi.org/10.1080/02690050500475476.

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Echenique, Pedro, Joseph R. Manson, Thomas L. Ferrell, and Robert N. Compton. "Rufus Haynes Ritchie." Physics Today 71, no. 4 (April 2018): 65. http://dx.doi.org/10.1063/pt.3.3905.

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Hamilton, Joseph, Wendall Holladay, William H. Kelly, and Aaron Galonsky. "Sherwood K. Haynes." Physics Today 44, no. 5 (May 1991): 80. http://dx.doi.org/10.1063/1.2810125.

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Bause, George S. "Haynes' Arabian Balsam." Anesthesiology 115, no. 4 (October 1, 2011): 803. http://dx.doi.org/10.1097/aln.0b013e31823592e0.

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Adam, Benjamin, Julie Tucker, and Graham Tewksbury. "Hot deformation data for Haynes 214, Haynes 230 and Inconel 740H." Data in Brief 28 (February 2020): 104923. http://dx.doi.org/10.1016/j.dib.2019.104923.

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Stephen Haynes, Jackie. "Interview: Jackie Stephen-Haynes." British Journal of Community Nursing 16, Sup9 (September 2011): S44—S46. http://dx.doi.org/10.12968/bjcn.2011.16.sup9.s44.

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Gabe, D. "Don Haynes (1923 – 2010)." Transactions of the IMF 88, no. 4 (July 2010): 174. http://dx.doi.org/10.1179/imf.2010.88.4.174.

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Lawrence, Walter. "BOYD WITHERS HAYNES, MD." Transactions of the ... Meeting of the American Surgical Association 123, &NA; (2005): 334–35. http://dx.doi.org/10.1097/00153307-200501230-00043.

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Hardy, Douglas S. "A Response to Haynes." Journal of Psychology and Theology 28, no. 4 (December 2000): 280–81. http://dx.doi.org/10.1177/009164710002800406.

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Hunt, Jamer. "Safe, Todd Haynes (1995)." Design and Culture 1, no. 2 (July 2009): 204–6. http://dx.doi.org/10.2752/175470709x12450568847659.

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Dissertations / Theses on the topic "Haynes"

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Rådberg, Malin. "Design of Experiment for Laser cutting in Superalloy Haynes 282." Thesis, Karlstads universitet, Science, Mathematics and Engineering Education Research (SMEER), 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kau:diva-44516.

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This project aims to investigate the effect of varying different laser cutting parameters on the laser cut surface. The parameters that were varied were cutting speed, beam effect, gas pressure and focal point. The statistical method Design of Experiment was used to plan the experiments and two full factorial test plans were set up, one with argon as cooling and protective gas and one with nitrogen. Sheet metal consisting of the superalloy HAYNES ® 282 with a thickness of 2,54 mm was investigated. Samples from the material were cut with different laser cutting parameters according to the test plans. The samples were evaluated by measuring cracks, recast layer thickness, surface irregularity, burr height and distance to beam deflection point on the cut surface. The resulting data was inserted as responses into the statistical program Modde 10.1 for analysis. Modde 10.1 provided models of high significance for the responses of Recast layer, Tav; Recast layer, Tmax; Burrheight, max and Distance to deflection point for the argon series and Recast layer, Tav and Recast layer, Tmax for the nitrogen series. The results showed that both recast layer thickness and burr height decreases with increased values of cutting speed, gas pressure and focal point as well as decreased values of beam effect within the parameter window investigated. They also showed that distance to deflection point increased with increasing values of gas pressure and focal point and with decreased values of cutting speed and beam effect within the parameter window. The results also showed that for the samples cut with argon as cooling and assistant gas the parameters that affects the recast layer thickness the most are focal point and gas pressure, whereas for the nitrogen series it is gas pressure and beam effect. The parameter with greatest effect on burr height is the cutting speed and for the distance to deflection point it is focal point and gas pressure that have the greatest effect. When comparing the argon and the nitrogen series to each other it can be seen that the argon series generate less recast layer from the entry of the cut until between 60 – 80 % into the cut, after which the argon series bypasses the nitrogen series in amount of recast layer produced in the cutting process in the majority of the places measured.
Projektet syftar till att undersöka effekten på den laserskurna ytan då laserskärningsparametrar varieras. Parametrarna som varierades var skärhastighet, lasereffekt, gastryck och fokalpunkt. Den statistiska metoden Design of Experiments användes för att planera experimenten. Två stycken fullskaligt faktoriella försöksplaner skapades, en med argon som skärgas och en med kväve som skärgas. Undersökningen gjordes på plåt bestående av superlegeringen HAYNES ® 282 med en tjocklek på 2,54 mm. Provbitar från materialet skars ut utifrån försöksplanerna med olika laserinställningar under skärprocessen. Provbitarna utvärderades genom att mäta sprickor, tjockleken på det omsmälta materialet, ytojämnheten, gradhöjden och avståndet till laserstrålens avböjningspunkt på den laserskurna ytan. Resultaten användes för analys i det statistiska programmet Modde 10.1. Modde 10.1 bidrog med modeller av hög signifikans för responserna Recast layer, Tav; Recast layer, Tmax; Burrheight, max and Distance to deflection point för argonserien och Recast layer, Tav och Recast layer, Tmax för kväveserien. Resultaten visar att både tjockleken på omsmält material och gradhöjden avtar med ökande värden på skärhastighet, gastryck och fokalpunkt samt minskande värden på lasereffekt inom det undersökta parameterfönstret. De visade också att till laserstrålens avböjningspunkt på den laserskurna ytan ökade med ökande värden på gastryck och fokalpunkt och med minskande värden på skärhastighet och lasereffekt inom parameterfönstret. Resultaten visade också att de parametrar som i störst utsträckning påverkar tjockleken på det omsmälta materialet för provbitarna i argonserien är fokalpunkt och gastryck, medan det för kväveserien är gastryck och lasereffekt. Parametern som har högst inverkar på gradhöjden är skärhastigheten, medan fokalpunkt och gastryck har störst effekt på avståndet till laserstrålens avböjningspunkt på den laserskurna ytan. Om kväveserien och argonserien jämförs med varandra kan det observeras att argonserien generellt genererar mindre omsmält material än kväveserien från det att laserstrålen träder in i materialet till dess att den är mellan 60 och 80 % in i snittet, vartefter argonserien går förbi kväveserien i mängd omsmält material på majoriteten av mätställen.
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Hirko, Jeffrey George. "CONDUIT ORIGIN AND PALEOHYDROLOGY OF HAYNES CAVE: MONROE COUNTY, WEST VIRGINIA." University of Akron / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=akron1336097022.

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Osoba, Lawrence. "A study on laser weldability improvement of newly developed Haynes 282 superalloy." Material Characterization Vol. 65(2012), p. 93 - 99, 2012. http://hdl.handle.net/1993/8156.

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Haynes alloy 282 is a new gamma prime (γ’) precipitation strengthened nickel-base superalloy developed for high temperature applications in land-based and aero turbine engines. Joining is a crucial process both during the manufacturing of new components and repair of service-damaged turbine parts. Unfortunately, the new superalloy cracks during laser beam welding (LBW), which is an attractive technique for joining superalloys components due to its low heat input characteristic that preclude the geometrical distortion of welded components. This research is therefore initiated with the goal of studying and developing an effective approach for preventing or minimizing cracking during LBW of the new superalloy Haynes 282. Careful and detailed electron microscopy and spectroscopy study reveal, for the first time, the formation of sub-micron grain boundary M5B3 particles, in the material. Microstructural study of welded specimens coupled with Gleeble thermo-mechanical physical simulations shows that the primary cause of weld heat affected zone (HAZ) cracking in the alloy is the sub-solidus liquation reaction of intergranular M5B3 borides in the material. Further weldability study showed that the HAZ liquation cracking problem worsens with reduction in welding heat input, which is normally necessary to produce the desired weld geometry with minimum distortion. In order to minimize the HAZ cracking during low heat input laser welding, microstructural modification of the alloy by heat treatment at 1080 - 1100oC has been developed. The pre-weld heat treatment minimizes cracking in the alloy by reducing the volume fraction of the newly identified M5B3 borides, while also minimizing non-equilibrium grain boundary segregation of boron liberated during dissociation of the boride particles. Further improvement in resistance to cracking was produced by subjecting the material to thermo-mechanically induced grain refinement coupled with a pre-weld heat treatment at 1080oC. This approach produces, for the first time, crack-free welds in this superalloy, and the benefit of this procedure in preventing weld cracking in the new material is preserved after post-weld heat treatment (PWHT), as additional cracking was not observed in welded specimens subjected to PWHT.
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Deutschländer, Robert [Verfasser], Michael [Gutachter] Pauen, John-Dylan [Gutachter] Haynes, and Albert [Gutachter] Newen. "Alltagsintuitionen zur Willensfreiheit / Robert Deutschländer ; Gutachter: Michael Pauen, John-Dylan Haynes, Albert Newen." Berlin : Humboldt-Universität zu Berlin, 2018. http://d-nb.info/1185175091/34.

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Veverková, Jana. "Effects of long-term high temperature exposure on the microstructure of haynes alloy 230." Thesis, University of Leicester, 2010. http://hdl.handle.net/2381/8333.

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Haynes Alloy 230 is a nickel-based sheet material used for combustor components in a number of small industrial gas turbines manufactured by Siemens. During normal operating service the material is subjected to high temperatures and cyclic mechanical and thermal stresses, which can lead to degradation of the microstructure and mechanical properties of the alloy, and hence limit component design life. This PhD thesis describes studies of the effects of long-term high temperature exposure on hardness and microstructural changes in creep rupture tested and thermally exposed samples of HA230. Advanced FEGSEM was used for documentation of the microstructural evolution in the temperature range of 500-1170°C following exposure up to 30000 hours. For identification of alloy phases, which could potentially act as indicators of the average exposure temperatures experienced for specific service periods, XRD and analytical TEM techniques were used. Primary carbides M12C and secondary carbides, M12C and M23C6, were identified. No TCP phases were observed within the microstructure of the tested samples, but the secondary M23C6 forms large ‘pool-like’ precipitates’ above 990°C which are very hard and brittle and could be detrimental for the material (e.g. reductions in ductility, high temperature strength). A hardness and microstructurally based model was used for the assessment of an ex-service HA230 transition duct and could be an aid for evaluation of the remnant life of HA230 combustor components. The tests were carried out as part of the COST 538 technology programme between 2004 and 2009.
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Frye, Matthew. "Influential Factors on Historic Interpretation: A Case Study of Tipton-Haynes State Historic Site." Digital Commons @ East Tennessee State University, 2020. https://dc.etsu.edu/etd/3718.

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Influences on the interpretation of Tipton-Haynes State Historic Site have caused many alterations to the site and the presentation of its history. Scholars have described how public history sites have continually expanded their interpretations as growing desires and interests from external influences such as the general public, state agencies, and donors. However, Tipton-Haynes has also faced many internal influences. While the creators of the site aided in the limitation and exclusion of the site’s vital history, over time the involvement and opinions of the board of trustee members, directors, and staff shaped an increasingly inclusive and expansive interpretation of the site. Therefore, the experience at Tipton-Haynes suggests that scholars should also consider the innerworkings of a historic site and the opinions of not just the community but also the opinions and choices of the people involved in the site and its creation. The inclusivity allows for a more expansive history while also creating new connections between the history of Tipton-Haynes and the general public.
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Rodelas, Jeffrey M. "Friction Stir Processing of Nickel-base Alloys." The Ohio State University, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=osu1341512683.

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Bogler, Carsten [Verfasser], John-Dylan [Akademischer Betreuer] Haynes, Philipp [Akademischer Betreuer] Sterzer, and Peter [Akademischer Betreuer] König. "Saliency processing in the human brain / Carsten Bogler. Gutachter: John-Dylan Haynes ; Philipp Sterzer ; Peter König." Berlin : Humboldt Universität zu Berlin, Mathematisch-Naturwissenschaftliche Fakultät II, 2014. http://d-nb.info/1058645048/34.

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Trabelsi, Mariem. "Propagation de fissures en fatigue oligocyclique multiaxiale à haute température pour le superalliage HAYNES® 188." Thesis, Paris Sciences et Lettres (ComUE), 2019. http://www.theses.fr/2019PSLEM952.

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Cette étude s’inscrit dans le cadre du projet ANR SEMAFOR (ANR-14-CE07-0037) (Simulation et caractérisationExpérimentale de la FissuratiOn en plasticité généRalisée) en partenariat avec l’ONERA, LMT Cachan et SAFRAN. Sous les conditions de hautes températures, certaines pièces aéronautiques subissent des chargements sévères nécessitant de prendre en compte la propagation de fissures de fatigue pour optimiser le dimensionnement et la sécurité des pièces. L’intensité des chargements et des températures provoquent une forte plastification dans la zone de propagation de fissures. Le matériau de l’étude est un superalliage à base de Cobalt, le HAYNES® 188, utilisé principalement pour les chambres de combustion aéronautiques. Cette étude consiste à caractériser expérimentalement la propagation de fissure en fatigue oligocyclique sous sollicitations biaxiales. La conception d’un essai original de propagation de fissure à haute température est développée pour des chargements biaxiaux coplanaires. Un inducteur de type pancake a été conçu afin de réduire le gradient thermique dans la zone centrale de l’éprouvette. Ce dispositif a été utilisé pour construire une étude approfondie d’essais biaxiaux dans les conditions de fatigue oligocyclique à haute température. Les mesures des champs de température par thermographie infra-rouge et une méthodologie expérimentale ont ainsi été mises en place afin d’appréhender au mieux les conditions de propagation de fissure. La détermination expérimentale des vitesses de propagation de fissures est l’un des objectifs majeurs de l’étude. Les essais ont été modélisés à l’aide de calculs par éléments finis. Un post-processeur, sans insertion de fissure, a permis de valider un modèle macroscopique de propagation de fissure basé sur des grandeurs énergétiques. A l’aide d’outils de remaillage conforme, la propagation de fissure a été modélisée par introduction explicite de la fissure observée expérimentalement. Cette démarche a permis d’analyser les grandeurs mécaniques pilotant la propagation de fissure de fatigue sous les conditions de plasticité étendue à haute température, afin d’établir des outils de modélisation 3D de propagation de fissure explicite
This study is concerned with the SEMAFOR (ANR-14-CE07-0037) project in collaboration with ONERA, Mines ParisTech,LMT Cachan and Safran. In very high temperature condition, as found for some engine aircraft components, crack couldinitiate near perforated zones. Once a crack is initiated, further degradation by crack growth is the result of a complex setof phenomena: multiaxial fatigue loading, thermal gradients and large scale yielding under oxidizing environment. The purpose of this study is to analyse the fatigue crack growth of the superalloy HAYNES® 188 under such conditions wit hbiaxial tests. The design of an original experiment is a challenging issue to conduct biaxial tests at high temperature. A specific inductor (pancake) was designed to decrease thermal gradient within the gage length. Subsequent thermalfield has been measured using Infra-red thermography. An experimental methodology was developped to ensure a deep analysis of the crack growth. One of our major purpuse is the determination of the experimental fatigue crack growth rate in such conditions. A finite element numerical analysis was achieved using a post-processing methodology based onenergy partition. This model has been successfully validated, at first without crack insertion, for cruciform specimen tests with neither modification of the model constitutive parameters. Using consistent remeshing tools, crack propagation was modeled by explicit introduction of the crack observed experimentally. This approach leads to analyze the mechanical quantities controlling the fatigue crack growth under large scale yielding at high temperature, in order to establish tools for3D modeling of explicit crack propagation
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Graneix, Jérémie. "Étude du soudage LASER Yb : YAG homogène et hétérogène des superalliages Hastelloy X et Haynes 188." Thesis, Toulouse, INPT, 2015. http://www.theses.fr/2015INPT0114/document.

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De nos jours, la complexité des pièces mécaniques est de plus en plus grande dans de nombreux secteurs industriels de pointes tels que l’aéronautique, l’aérospatiale ou bien encore le domaine médical. Pour répondre à ces nouvelles exigences, notamment en termes de géométrie, de nouvelles techniques de conception et de fabrication automatisées intègrant également une meilleure traçabilité des pièces, sont mises en place. Ce travail de thèse s’est inscrit dans un projet partenarial entre le Laboratoire Génie de Production de l’ENIT et la société EXAMECA, spécialiste de pièces chaudronnées pour l’aéronautique. L’étude a porté plus précisément sur l’assemblage permanent de pièces en superalliages par soudage LASER pour la réalisation d’une nouvelle chambre de combustion de turbomachine. Les assemblages des différentes parties de la chambre de combustion sont actuellement réalisés par procédé TIG (Tungsten Inert Gas), encore appelé procédé GTAW (Gas Tungsten Arc Welding), de manière manuelle ou semi-automatique avec fil d’apport de la même nuance que le superalliage base nickel. Même si cette technique industrielle est éprouvée, elle peut générer encore des problèmes de non-conformité car elle requière une grande dextérité des opérateurs pour éviter notamment les déformations importantes des pièces chaudronnées. L’étude avait donc pour objectif d’évaluer la pertinence du procédé de soudage LASER Yb : YAG pour l’assemblage homogène et hétérogène des superalliages Hastelloy X et Haynes 188 sans métal d’apport. Le procédé de soudage autogène à l’aide d’une source LASER disque Yb : YAG est encore relativement récent dans l’industrie même s’il semble offrir de nouvelles perspectives intéressantes. Une première partie de l’étude a permis de caractériser la caustique du faisceau LASER afin de déterminer des paramètres clés lors du soudage que sont par exemple la forme et la taille du spot LASER, la répartition de la densité de puissance à la surface de la pièce ou au point focal par exemple. Cette étape finalisée, les domaines de soudabilité des assemblages homogènes des superalliages Hastelloy X et Haynes 188 et des assemblages hétérogènes Hastelloy X - Haynes 188 ont été déterminés. L’influence des principaux paramètres de soudage sur la géométrie (forme et taille) et la tenue mécanique des cordons a pu être identifiée. Des conditions optimales de soudage ont été établies pour les différentes conditions de soudage. Une étude métallurgique des cordons optimisés, obtenus pour les différentes configurations, a été menée à différentes échelles. Elle a permis de déterminer des relations entre d’une part, les paramètres et les modes de soudage (conduction ou keyhole) et d’autre part, entre les modes de soudage et les microstructures des différentes zones des cordons qui conditionnement leurs propriétés mécaniques
Nowadays, the complexity of mechanical parts is becoming more and more important in numerous cutting-edge insdustries such as aeronautics, aerospace or the medical field. To meet such new requirements, particulary in terms of geometry, innovative conception and automated manufacturing techniques, integrating as well a better traceability of parts, are implemented. This thesis is in partnership with The LGP (Laboratoire Génie de Production) of the National Engineering School of Tarbes (ENIT) and EXAMECA, a company specialized in boiler making for aerospace applications. The study essentially focused on permanent assembly of superalloy parts by LASER welding, in order to develop a new turbomachinery combustion chamber. Assembly of different parts of the combustion chamber are presently performed by TIG (Tungsten Inert Gas) process, or GTAW (USA : Gas Tungsten Arc Welding) process. This manufacturing phase is realized in a manual mode with semi-automatic equipment providing the wire with a similar grade as the nickel base superalloy. Even though this industrial process has been proven, it can still cause noncompliance issues because it requires great dexterity from operators to avoid important deformations of welded parts. Therefore, this study aimed at evaluating the relevance of LASER Yb : YAG welding process, for homogeneous and heterogeneous assembly of Hastelloy X and Haynes 188 superalloys, without filler metal. Autogeneous welding process associated with LASER Yb : YAG disc source is still relatively new in the industry even though it seems to offer very promising perspectives. A first part of the study is dedicated to LASER beam’s caustic characterization, in order to determine key parameters for welding, including shape and size of LASER spot, power density distribution on the surface or at focal point. Once this phase was completed, fields of weldability of homogeneous assemblies of Hastelloy X and Haynes 188 superalloys as well as heterogeneous assemblies of Hastelloy X / Haynes 188 have been determined. Impact of main welding parameters on geometry (shape and size) and mechanical strength beads were identifed. Optimal welding conditions have been established for different welding conditions. A metallurgical study on optimized beads, obtained for different configurations, has been carried out at different scales. It allowed determining relationships between parameters and welding modes (conduction or keyhole), but also between welding modes and microstructures of different beads areas that condition mechanical properties
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Books on the topic "Haynes"

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Todd Haynes. Urbana: University of Illinois Press, 2013.

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Haynes, Nancy. Nancy Haynes. New York: John Good Gallery, 1993.

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Kirili, Alain. Alain Kirili & Roy Haynes. Nantes: Ecole régionale des Beaux-Arts de Nantes, 1993.

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Storer, Jay. The Haynes welding manual. Somerset, England: Haynes Pub. Group, 1994.

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Haynes, John L. Haynes-McDonald heritage quest. Anchorage, Alaska (3026 Brittany Place, Anchorage 99504): J.L. Haynes, 1995.

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Storer, Jay. The Haynes welding manual. Somerset, England: Haynes Pub. Group, 1994.

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Pichon, Sandra Haynes. Dixie delights: Sandra Haynes Pichon. [Slidell? La.]: S.H. Pichon, 1994.

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Geller, Theresa L., and Julia Leyda, eds. Reframing Todd Haynes. Duke University Press, 2022. http://dx.doi.org/10.1215/9781478022626.

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For three decades, award-winning independent filmmaker Todd Haynes, who emerged in the early 1990s as a foundational figure in New Queer Cinema, has gained critical recognition for his outsider perspective. Today, Haynes is widely known for bringing women’s stories to the screen. Analyzing Haynes’s films including Safe (1995), Velvet Goldmine (1998), Far from Heaven (2002), and Carol (2015), as well as his unauthorized Karen Carpenter biopic, Superstar (1987), and the television miniseries Mildred Pierce (2011), the contributors to Reframing Todd Haynes reassess his work in light of his long-standing feminist commitments and his exceptional career as a director of women’s films. They present multiple perspectives on Haynes’s film and television work and on his role as an artist-activist who draws on academic theorizations of gender and cinema. The volume illustrates the influence of feminist theory on Haynes’s aesthetic vision, most evident in his persistent interest in the political and formal possibilities afforded by the genre of the woman’s film. The contributors contend that no consideration of Haynes’s work can afford to ignore the crucial place of feminism within it. Contributors. Danielle Bouchard, Nick Davis, Jigna Desai, Mary R. Desjardins, Patrick Flanery, Theresa L. Geller, Rebecca M. Gordon, Jess Issacharoff, Lynne Joyrich, Bridget Kies, Julia Leyda, David E. Maynard, Noah A. Tsika, Patricia White, Sharon Willis
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Clew, Jeff. Haynes. Haynes Publishing, 1988.

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L, Felperin. Todd Haynes on Todd Haynes. Faber & Faber, Incorporated, 2006.

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Book chapters on the topic "Haynes"

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Schroeder, David. "Roy Haynes." In From the Minds of Jazz Musicians, 95–100. New York, NY : Routledge, 2018.: Routledge, 2017. http://dx.doi.org/10.4324/9781315282572-17.

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Holliday, Vance T. "Haynes, Jr., C. Vance." In Encyclopedia of Global Archaeology, 4869–71. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-30018-0_349.

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Holliday, Vance T. "Haynes, Jr., C. Vance." In Encyclopedia of Global Archaeology, 3226–29. New York, NY: Springer New York, 2014. http://dx.doi.org/10.1007/978-1-4419-0465-2_349.

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Kathy, A. Perkins. "Interview with Edward Everett Haynes, Jr." In The Routledge Companion to African American Theatre and Performance, 269–71. New York, NY : Routledge, 2019. |: Routledge, 2018. http://dx.doi.org/10.4324/9781315191225-52.

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Fahrmann, M. G., and L. M. Pike. "Experimental TTT Diagram of HAYNES 282 Alloy." In Proceedings of the 9th International Symposium on Superalloy 718 & Derivatives: Energy, Aerospace, and Industrial Applications, 565–78. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-89480-5_37.

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Pike, L. M. "Long Term Thermal Exposure of HAYNES 282 Alloy." In Superalloy 718 and Derivatives, 644–60. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495223.ch50.

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Caron, Jeremy L. "Weldability and Welding Metallurgy of Haynes 282 Alloy." In 8th International Symposium on Superalloy 718 and Derivatives, 273–86. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2014. http://dx.doi.org/10.1002/9781119016854.ch23.

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Thau, Eric M. "All that Melodrama Allows: Sirk, Fassbinder, Almodóvar, Haynes." In World Cinema's 'Dialogues' with Hollywood, 188–200. London: Palgrave Macmillan UK, 2007. http://dx.doi.org/10.1057/9780230223189_12.

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Andersson, Joel, Göran Sjöberg, and Mahesh Chaturvedi. "Hot Ductility Study of HAYNES(®) 282(®) Superalloy." In Superalloy 718 and Derivatives, 538–54. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495223.ch41.

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Rao, K. Bhanu Sankara, M. G. Castelli, G. P. Allen, and J. R. Ellis. "Temperature Dependent Cyclic Deformation Mechanisms in Haynes 188 Superalloy." In Computational Mechanics ’95, 1359–64. Berlin, Heidelberg: Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-79654-8_220.

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Conference papers on the topic "Haynes"

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Katcher, Michael, and Dwaine L. Klarstrom. "A Review of Haynes® 230 and Haynes 617 Alloys for High Temperature Gas Cooled Reactors." In ASME 2007 Pressure Vessels and Piping Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/pvp2007-26656.

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HAYNES 230 and 617 alloys are competing for use on Generation IV, high temperature gas cooled reactor components because of their good high temperature creep strength in the temperature range of 760°C and 982°C and resistance to attack in the gas cooled reactor environment. A review of the metallurgy affecting the properties in each alloy is provided. It is shown that the grain size and carbide precipitation developed during manufacture affect short term and long term ductility, fatigue life, and creep strength. For example, 230 alloy has a finer grained structure which promotes fatigue strength with a slight sacrifice in creep strength. The 617 alloy has a coarser grain structure which provides slightly higher creep resistance while sacrificing some fatigue strength. Thermal aging also introduces gamma prime precipitation to 617 alloy in addition to grain boundary carbides. This, along with grain boundary oxidation, reduces the low cycle fatigue strength of 617 alloy compared to 230 alloy. Independent studies have shown that 230 alloy possesses higher resistance to thermal fatigue than 617 alloy. However, welds of both base metals with similar weld composition have about the same thermal fatigue life. Cooling rates from solution annealing temperatures during processing affect the ductility and creep strength of these alloys with the highest cooling rates preferred for retention of ductility and creep strength. Slow cooling rates promote carbide precipitation in the grain boundaries which reduces ductility and creep strength.
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Gowreesan, Vamadevan, Wayne Greaves, Yogi Pardhi, and Karen Barrios. "Microstructural Evolution of Wrought and AM Haynes 188 Under Long Term Thermal Exposure." In ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/gt2022-79113.

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Abstract Haynes 188 is a cobalt-based superalloy used in hot section gas turbine components due to its excellent oxidation resistance and elevated temperature stability. Parts made from Haynes 188 are traditionally manufactured from wrought or forged material. Additive manufacturing (AM) may be a less time consuming and more cost-effective alternative, particularly for replacement parts. Additionally, necessary design changes can be quickly introduced into service using additive manufacturing. It is important to understand the effect of long-term thermal exposure on additively manufactured parts before they are put into demanding high temperature applications. Data on the effect of long-term thermal exposure on wrought Haynes 188 is readily available in the open literature. However, such data for additively manufactured Haynes 188 is scarce. This paper discusses an experimental study that investigated the microstructural evolution in wrought and AM Haynes 188 under long-term thermal exposure. Optical metallography and scanning electron microscopy (SEM) were performed on wrought and AM Haynes 188 in the virgin and long-term thermally exposed conditions. Mechanical test samples from the coupons were then extracted and tested in both conditions. Lastly, the fracture surfaces of the mechanical test specimens were evaluated by SEM fractography and metallography of sections through the fracture surfaces. The findings help to understand how long-term thermal exposure affects the microstructure and mechanical properties of wrought and AM Haynes 188. Most importantly, it illustrates a significant difference in microstructural response of the two materials to long term thermal exposure and its effect on mechanical properties.
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Lee, S. Y., P. K. Liaw, Y. L. Lu, D. Fielden, L. M. Pike, and D. L. Klarstrom. "Elevated-Temperature Creep-Fatigue Crack-Growth Behavior of Nickel-Based HAYNES R-41, HAYNES 230 and HASTELLOY X Alloys." In Superalloys. TMS, 2008. http://dx.doi.org/10.7449/2008/superalloys_2008_509_514.

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Dreshfield, R. L. "Long Time Creep Rupture of Haynes Alloy 188." In Superalloys. TMS, 1996. http://dx.doi.org/10.7449/1996/superalloys_1996_383_389.

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Veverkova, J., A. Strang, G. R. Marchant, G. M. McColvin, and H. V. Atkinson. "High Temperature Microstructural Degradation of Haynes Alloy 230." In Superalloys. TMS, 2008. http://dx.doi.org/10.7449/2008/superalloys_2008_479_488.

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Pike, L. "Long Term Thermal Exposure of HAYNES 282 Alloy." In Superalloys. John Wiley & Sons, Inc., 2010. http://dx.doi.org/10.7449/2010/superalloys_2010_645_660.

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Caron, J. "Weldability and Welding Metallurgy of Haynes 282 Alloy." In Superalloys. John Wiley & Sons, Inc., 2014. http://dx.doi.org/10.7449/2014/superalloys_2014_273_286.

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Li, Yanmin, Yong Liu, and Henry Peng. "Laser net shape manufacturing of Haynes 188 alloy." In ICALEO® 2008: 27th International Congress on Laser Materials Processing, Laser Microprocessing and Nanomanufacturing. Laser Institute of America, 2008. http://dx.doi.org/10.2351/1.5061320.

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Lai, George Y. "Several Modern Wrought Superalloys for Gas Turbine Applications." In ASME 1996 Turbo Asia Conference. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-ta-030.

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The present paper discusses several modern wrought superalloys that are being used for various hot gas path components in modern gas turbines. HAYNES® 230™ alloy (Ni-22Cr-14W-2Mo) is used for combustors and transition pieces to replace an old combustor alloy, HASTELLOY® X alloy (Ni-22Cr-19Fe-9Mo), because of higher creep-rupture strength, better oxidation resistance, higher low-cycle fatigue resistance, and other improved properties. The alumina forming HAYNES 214™ alloy (Ni-16Cr-3Fe-4.5Al-Y) replaces HASTELLOY X for honeycomb seals because of its superior oxidation resistance. HAYNES 242™ alloy (Ni-8Cr-25Mo), strengthened by a long-range ordered phase Ni2(Cr,Mo) with low thermal expansion and high strength, is used for turbine casings and seal rings. A less expensive, nitride-strengthened Fe-Ni-Cr alloy, HAYNES HR-120™ alloy, offers an attractive upgrade to many stainless steels and some Ni-base alloys for less demanding, hot section components.
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Kirk, Tracey, Aaron Bowsher, and Peter Crudgington. "High Temperature Brush Seal Development." In ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gt2017-63091.

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The industry bristle material of choice for brush seals has been the cobalt-based alloy Haynes®25 (also known as L605) for over 30 years. Haynes®25 has excellent oxidation resistance and wear properties in brush seal applications up to temperature of 620°C [1148°F]. Above this temperature creep resistance becomes undesirable for brush seal bristles and has lead to alternative sealing solutions to be implemented in these turbine locations. Nickel-based alloys have been explored as an alternative for Haynes®25 but have been shown to gall badly and wear quickly in comparison. As increases in turbine performance have resulted in an increase in operating temperatures, it has lead to a need to find a bristle material that performs at temperatures above the limitation of Haynes®25. Initial experimental data has been obtained for a new cobalt-based alloy that shows potential for use as a bristle material at temperatures above 620°C [1148°F]. Further experimental results also indicate that the material appears to have better wear characteristics than Haynes®25 and may prove to be a feasible alternative in some cases. This paper outlines a material selection process for brush seals, along with development of the alloy for use within brush seals and details of the comparative testing carried out at Cross Manufacturing Company.
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Reports on the topic "Haynes"

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Chaudhury, Prabir, and Dan Zhao. Atlas of Formability; Haynes 230. Fort Belvoir, VA: Defense Technical Information Center, August 1992. http://dx.doi.org/10.21236/ada268325.

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Karmiol, Benjamin. Etch Rates Haynes 25 and 304L Stainless Steel. Office of Scientific and Technical Information (OSTI), March 2022. http://dx.doi.org/10.2172/1856141.

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Pattrick Calderoni. Hydrogen Permeability of Incoloy 800H, Inconel 617, and Haynes 230 Alloys. Office of Scientific and Technical Information (OSTI), July 2010. http://dx.doi.org/10.2172/989876.

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Antoun, Bonnie, and Harumichi Kariya. Milestone Report: Effect of High Temperature CO2 on Haynes 230 Alloy. Office of Scientific and Technical Information (OSTI), November 2020. http://dx.doi.org/10.2172/1817975.

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Kariya, Harumichi, and Bonnie Antoun. Effect of High Temperature CO2 on Haynes 230 Alloy (Updated Jan 2021). Office of Scientific and Technical Information (OSTI), January 2021. http://dx.doi.org/10.2172/1763860.

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Shingledecker, J. P., D. B. Glanton, R. L. Martin, B. L. Sparks, and R. W. Swindeman. Tensile and Creep-Rupture Evaluation of a New Heat of Haynes Alloy 25. Office of Scientific and Technical Information (OSTI), February 2007. http://dx.doi.org/10.2172/901496.

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Emswiler, T. R. Phase I decontamination of the J. C. Haynes site, Newark, Ohio. Final report. Office of Scientific and Technical Information (OSTI), November 1985. http://dx.doi.org/10.2172/6458943.

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Shingledecker, J. P., D. B. Glanton, R. L. Martin, B. L. Sparks, and R. W. Swindeman. Tensile and Creep-Rupture Evaluation of a New Heat of Haynes Alloy 25. Office of Scientific and Technical Information (OSTI), February 2007. http://dx.doi.org/10.2172/921772.

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Richard N. Wright. Summary of Studies of Aging and Environmental Effects on Inconel 617 and Haynes 230. Office of Scientific and Technical Information (OSTI), September 2006. http://dx.doi.org/10.2172/911722.

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Kirka, Michael M., Kinga A. Unocic, Keith Kruger, and Alison Forsythe. Process Development for Haynes® 282® Using Additive Manufacturing. Office of Scientific and Technical Information (OSTI), March 2018. http://dx.doi.org/10.2172/1435227.

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