Modeling of shrinkage during investment casting of thin-walled hollow turbine blades
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DOI: 10.1016/j.jmatprotec.2017.01.005
Abstract: Abstract The shrinkage ratio is a key parameter in designing the investment casting die for hollow turbine blades of high-performance aircraft engines. To avoid extensive modifications to the die shape, we took a single-crystal hollow… read more here.
Keywords: turbine blades; shrinkage; investment casting; hollow turbine ... See more keywords