SAE Technical Paper Series 1966
DOI: 10.4271/660055
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The Control of Grain Shape and Its Effect on the Properties of Cast Components for High-Temperature and High-Stress Applications

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“…Aircraft-engine turbine blades were produced by a variant of the exomold technique by Piearcey and VerSnyder (1966). They directionally solidified blades of alloy Mar-M200 by casting the alloy into a preheated mold positioned on a copper chill.…”
Section: Directional Solidification Of High-temperature Alloysmentioning
confidence: 99%
“…Aircraft-engine turbine blades were produced by a variant of the exomold technique by Piearcey and VerSnyder (1966). They directionally solidified blades of alloy Mar-M200 by casting the alloy into a preheated mold positioned on a copper chill.…”
Section: Directional Solidification Of High-temperature Alloysmentioning
confidence: 99%