DocumentCode
2421828
Title
Ab-initio Molecular Dynamics Simulations of Molten Ni-Based Superalloys
Author
Woodward, Christopher ; Asta, Mark ; Trinkle, Dallas R. ; Lill, James ; Angioletti-Uberti, Stefano
Author_Institution
US Air Force Res. Lab., Wright Patterson AFB, OH
fYear
2008
fDate
14-17 July 2008
Firstpage
169
Lastpage
174
Abstract
Variations in composition and temperature of the liquid-phase molar volume (V(c,T)) play a critical role in driving convective instabilities during the casting of single-crystal turbine blades. These instabilities have long been associated with the formation of large highly mis-oriented grains (i.e., freckle defects) that produce significant degradation in materials properties of these critical aerospace components. Ab initio molecular dynamics (AIMD) simulations have been performed for elemental, binary and ternary alloys of Ni with Al, W, Re, and Ta, as well as a RENE-N4 multi-component superalloy, to compute equations of state at 1830 and 1750 K. Where comparisons with measurements are available, AIMD-calculated volumes agree to within 0.6-1.8% of experiment. Results are compared with recently published parameterizations of V(c,T) developed using binary experimental data from a narrow range of compositions. Also, structural analysis of the AIMD results based on radial distribution functions augmented with common-neighbor analysis and bond angle distributions reveal a strong tendency for icosahedral short range order for Ni-W and Ni-Re alloys. Finally, a new constant pressure methodology was added to the AIMD package that has allowed the efficient simulation of highly complex alloys, such as an eight component model of a RENE-N4 Ni-based superalloy.
Keywords
ab initio calculations; aerospace components; aluminium alloys; blades; casting; equations of state; molecular dynamics method; nickel alloys; rhenium alloys; superalloys; tantalum alloys; tungsten alloys; turbines; NiAl; NiRe; NiTa; NiW; RENE-N4 multicomponent superalloy; ab-initio molecular dynamics simulations; aerospace components; bond angle distributions; casting; driving convective instability; equations of state; freckle defects; liquid-phase molar volume; nickel-based superalloys; single-crystal turbine blades; structural analysis; temperature 1750 K; temperature 1830 K; Aerodynamics; Aerospace components; Blades; Casting; Computational modeling; Degradation; Material properties; Performance evaluation; Temperature; Turbines;
fLanguage
English
Publisher
ieee
Conference_Titel
DoD HPCMP Users Group Conference, 2008. DOD HPCMP UGC
Conference_Location
Seattle, WA
Print_ISBN
978-1-4244-3323-0
Type
conf
DOI
10.1109/DoD.HPCMP.UGC.2008.15
Filename
4755860
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