2001
DOI: 10.1034/j.1600-0692.2001.300504.x
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Thermodynamics of liquid and undercooled liquidAl–Cr–Ni alloys

Abstract: The partial and the integral enthalpies of mixing of liquid ternary Al–Cr–Ni alloys have been determined by high temperature iso‐peribolic calorimetry at 1718–1731 K. Measurements for ternary alloys were performed along 4 isopleths with xCr:xNi of 0.20:0.80, 0.50:0.50, 0.70:0.30, and 0.85:0.15. The results were analytically described by the thermodynamically adapted power series according to the Kohler interpolation geometry as well as by the regular association model using the parameters for the constituent b… Show more

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Cited by 7 publications
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“…[110][111][112] Further thermodynamic data can be obtained by measuring the enthalpies of dissolution of elements in liquid Al. …”
Section: 100mentioning
confidence: 99%
See 1 more Smart Citation
“…[110][111][112] Further thermodynamic data can be obtained by measuring the enthalpies of dissolution of elements in liquid Al. …”
Section: 100mentioning
confidence: 99%
“…109 Enthalpies of mixing of liquid phases are measured by high temperature calorimetry. [110][111][112] Further thermodynamic data can be obtained by measuring the enthalpies of dissolution of elements in liquid Al. …”
Section: Melting and Incipient Meltingmentioning
confidence: 99%
“…The value of the surface tension calculated by assuming ideal mixing and taking the surface tension values of the alloy components at their melting points as given by Keene [14] is obtained as r(T l ) = 1.679 ± 0.025 Nm -1 which is lower than the value of r(T l ) = 1.79 ± 0.05 Nm -1 from this experiment. This comparison, however, neglects the large differences in the melting points of the individual alloy components, the influence of dissolved oxygen, the non-ideality of the alloy compositon [15] or the formation of compounds, [16] and the possibility of surface segregation. [17] Recently, two experiments by the sessile drop method by Hayashi [18] et al and by Ricci [19] et al have provided values of r(T l ) = 1.97 Nm -1 and r(T l ) = 1.…”
Section: Surface Tensionmentioning
confidence: 99%
“…Cr-and Ni-based superalloys have excellent hightemperature strength, good corrosion resistance, low thermal expansion and are suitable for high performance aerospace, automobile and power plant applications. The Al-Cr and Cr-Ni systems have been studied extensively as constituents of complex superalloys based on the Al-Cr-Ni system [5]. Indeed, the AlNi-Cr-Ni subsection is a model system for superalloys [6].…”
Section: Introductionmentioning
confidence: 99%