Evaluation of two nickel-base alloys, alloy 713C and NASA TAZ-8A, produced by extrusion of prealloyed powders
Extruded prealloyed powder evaluation for two nickel-base alloys
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Extruded prealloyed powder evaluation for two nickel-base alloys
White powder compounds of metal oxides for thermal protective coating of spacecraft
Dispersion strengthened nickel produced from ultrafine comminuted powders
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Density and particle size effects on complex dielectric constant of basalt powders in X and K bands
Prealloyed powders of Ni base alloys, Alloy 713C and NASA TAZ-8A made by inert gas atomization for improved strength and ductility
Ni dispersion-strengthened composites from ultrafine comminuted powders, describing forming techniques and test results
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Tensile and stress rupture tests of Co base alloy bars extruded from prealloyed powders made by Ar gas atomization
Apollo 11 lunar fines and ground terrestrial mafic rock powders effective surface areas and heats of adsorption, using Brunauer-Emmett-Teller Kr adsorption method
A small displacement-small strain finite element technique utilizing the constant strain triangle and incremental constitutive equations for elasticplastic (media nonhardening and obeying a Coulomb yield condition) was applied to the analysis of gravity flow initiation. This was done in a V-shaped hopper containing a powder under lunar environmental conditions. Three methods of loading were examined. Of the three, the method of computing the initial state of stress in a filled hopper prior to drawdown, by adding material to the hopper layer by layer, was the best. Results of the analysis of a typical hopper problem show that the initial state of stress, the elastic moduli, and the strength parameters have an important influence on material response subsequent to the opening of the hopper outlet.