An Integrated Approach to Relate Hot Forging Process Controlled Microstructure of IN718 Aerospace Components to Fatigue Life

B. Pieraggi and J.F. Uginet, “Fatigue and Creep Properties in Relation with Alloy 718 Microstructure”, Superalloys 718, 625, 706 and Various Derivatives, (1994), 535–544.
Google Scholar
E. Andrieu, R. Cozar and A. Pineau, “Effect of Environment and Microstructure on the High Temperature Behaviour of Alloy 718”, Superalloy 718-Metallurgy and Applications, (1989), 241–256.
Google Scholar
J.M. Zhang et.al., “Effect of Hot Deformation Parameters on the Grain Size of Wrought IN718”, Superalloys 718, 625, 706 and Various Derivatives, (1997), 183–192.
Google Scholar
G.E. Korth, “Effects of Various Parameters on the Fatigue Life of Alloy 718”, Superalloys 718, 625 and Various Derivatives, (1991), 457–476.
Google Scholar
L. Shuqi et.al., “The Effect of d-Phase on Crack Propagation under Creep and Fatigue Conditions in Alloy 718”, Superalloys 718, 625, 706 and Various Derivatives, (1994), 545–555.
Google Scholar
P.E. Mosser et.al., “Metallurgical Aspects of Forge Modelling in Alloy 718”, Superalloy 718-Metallurgy and Applications, (1989), 179–188.
Google Scholar
M. Stoschka et.al., “Assessment of Lifetime Calculation of Forged IN718 Aerospace Components Based on a Multi-Parametric Microstructural Evaluation”, Superalloys 2008, 573–582.
Google Scholar
J.F. Uginet and B. Pieraggi, “Study of Secondary Grain Growth on 718 Alloy”, Superalloys 718, 625, 706 and Various Derivatives, (1997), 343–352.
Google Scholar
H. Maderbacher et.al. “Link from the Microstructure to the Fatigue Lifetime of Forged Inconel 718 Components”, Danubia-Adria Symposium on Advances in Experimental Mechanics, 26 (2009), 59–60.
Google Scholar
W. Eichlseder and B. Unger, “Prediction of the fatigue life with the finite element method”, SAE Paper, 940245 (1994).
10.4271/940245
Google Scholar
N. Kawagaishi, Q. Chen and H. Nisitani, “Fatigue Strength of Inconel 718 at Elevated Temperatures”, Fatigue Fracture Engineering Material Structures, 23 (2000), 209–216.
10.1046/j.1460-2695.2000.00263.x
Google Scholar
M. Stockinger et.al., “Modeling of DELTA-Phase Dissolution During Preheating of INCONEL718 Turbine Disks”, Symposium on Superalloys 718, 625, 706 and Derivatives, (2001), 141–148.
Google Scholar
M. Stockinger and J. Tockner, “Optimizing the Forging of Critical Aircraft Parts by the Use of Finite Element Coupled Microstructure Modeling”, Superalloys 718, 625, 706 and Derivatives, (2005), 517–526.
Google Scholar

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An Integrated Approach to Relate Hot Forging Process Controlled Microstructure of IN718 Aerospace Components to Fatigue Life

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An Integrated Approach to Relate Hot Forging Process Controlled Microstructure of IN718 Aerospace Components to Fatigue Life

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