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Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

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This is a second Triennial Conference on the physical, chemical, <strong>and</strong> mechanical properties of materials, interpreted to mean<br />

simple <strong>and</strong> complex inorganic solids, i.e., metals, semiconductors, <strong>and</strong> mineral of technological <strong>and</strong> environmental significance.<br />

DTIC<br />

Alloys; Minerals; Semiconductors (Materials); Metals<br />

<strong>2000</strong>0064094 NASA Glenn Research Center, Clevel<strong>and</strong>, OH USA<br />

Effects of Melt Convection <strong>and</strong> Solid Transport on Macrosegregation <strong>and</strong> Grain Structure in Equiaxed Al-Cu Alloys<br />

Rerko, Rodney S., Iowa Univ., USA; deGroh, Henry C., III, NASA Glenn Research Center, USA; Beckermann, Christoph, Iowa<br />

Univ., USA; May <strong>2000</strong>; 118p; In English<br />

Contract(s)/Grant(s): RTOP 101-13-0A<br />

Report No.(s): NASA/TM-<strong>2000</strong>-210020; E-12217; NAS 1.15:210020; No Copyright; Avail: CASI; A06, Hardcopy; A02, Microfiche<br />

Macrosegregation in metal casting can be caused by thermal <strong>and</strong> solutal melt convection, <strong>and</strong> the transport of unattached solid<br />

crystals resulting from nucleation in the bulk liquid or dendrite fragmentation. to develop a comprehensive numerical model for<br />

the casting of alloys, an experimental study has been conducted to generate benchmark data with which such a solidification model<br />

could be tested. The objectives were: (1) experimentally study the effects of solid transport <strong>and</strong> thermosolutal convection on<br />

macrosegregation <strong>and</strong> grain size; <strong>and</strong> (2) provide a complete set of boundary conditions temperature data, segregation data, <strong>and</strong><br />

grain size data - to validate numerical models. Through the control of end cooling <strong>and</strong> side wall heating, radial temperature gradients<br />

in the sample <strong>and</strong> furnace were minimized. Thus the vertical crucible wall was adiabatic. Samples at room temperature were<br />

24 cc <strong>and</strong> 95 mm long. The alloys used were Al-1 wt. pct. Cu, <strong>and</strong> Al- 10 wt. pct. Cu; the starting point for solidification was<br />

isothermal at 710 <strong>and</strong> 685 C respectively. to induce an equiaxed structure various amounts of the grain refiner TiB2 were added.<br />

Samples were either cooled from the top, or the bottom. Several trends in the data st<strong>and</strong> out. In attempting to model these experiments,<br />

concentrating on these trends or differences may be beneficial.<br />

Author<br />

Melts (Crystal Growth); Convection; Solidification; Transport Properties; Aluminum Alloys; Copper; Experimentation; Grain<br />

Size; Temperature Gradients; Free Convection; Fragmentation<br />

<strong>2000</strong>0064095 Case Western Reserve Univ., Clevel<strong>and</strong>, OH USA<br />

Thermophysical Properties of GRCop-84 Final Report<br />

Ellis, David L., Case Western Reserve Univ., USA; Keller, Dennis J., RealWorld Quality Systems, Inc., USA; June <strong>2000</strong>; 22p;<br />

In English<br />

Contract(s)/Grant(s): NAS3-463; RTOP 242-23-54<br />

Report No.(s): NASA/CR-<strong>2000</strong>-210055; E-12257; NAS 1.26:210055; No Copyright; Avail: CASI; A03, Hardcopy; A01, Microfiche<br />

The thermophysical properties <strong>and</strong> electrical resistivity of GRCop-84 (Cu - 8 at.% Cr-4 at.% Nb) were measured from cryogenic<br />

temperatures to near its melting point. The data were analyzed using weighted regression to determine the properties as a<br />

function of temperature <strong>and</strong> assign appropriate confidence intervals. The results showed that the thermal expansion of GRCop-84<br />

was significantly lower than NARloy-Z (Cu-3 wt. % Ag-0.5 wt. % Zr), the currently used thrust cell liner material. The lower<br />

thermal expansion is expected to translate into lower thermally induced stresses <strong>and</strong> increases in thrust cell liner lives between<br />

2X <strong>and</strong> 41X over NARloy-Z. The somewhat lower thermal conductivity of GRCop-84 can be offset by redesigning the liners to<br />

utilize its much greater mechanical properties. Optimized designs are not expected to suffer from the lower thermal conductivity.<br />

Electrical resistivity data, while not central to the primary application, show that GRCop-84 has potential for applications where<br />

a combination of good electrical conductivity <strong>and</strong> strength is required.<br />

Author<br />

Copper Alloys; Chromium Alloys; Thermophysical Properties; Electrical Resistivity; Measure <strong>and</strong> Integration; Cryogenic Temperature<br />

<strong>2000</strong>0064902 NASA Lewis Research Center, Clevel<strong>and</strong>, OH USA<br />

Thermal Studies of New Precursors to Indium-tin Oxides for Use as Sensor Materials in the Detection of NO(x)<br />

Goldsby, J. C., NASA Lewis Research Center, USA; Kacik, T., NASA Lewis Research Center, USA; Hockensmith, C. M.; Thermochimica<br />

Acta; 1999; ISSN 0040-6031; <strong>Volume</strong> 340-1, pp. 315-322; In English; Copyright; Avail: Issuing Activity<br />

Control of combustion product emissions in both sub <strong>and</strong> super-sonic jet engines can be facilitated by measurement of NO(x)<br />

levels with metal oxide sensors, In2O3, metal-doped SnO2, <strong>and</strong> SnO, (as well as other materials) show resistivity changes in the<br />

presence of NO(x), but often their sensitivity, stability, <strong>and</strong> selectivity are low. This study was designed to develop new synthetic<br />

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