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STRUCTURE AND PROPERTIES OF THE WORKING BLADES OF AIRCRAFT GAS TURBINE ENGINES MADE OF HEAT-RESISTANT NICKEL ALLOY ZhS32-VI

Authors: Sergey Puchek, Sergey Belikov

Publication: Casting processes

Published: Sep 7, 2026

Source: Crossref

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STRUCTURE AND PROPERTIES OF THE WORKING BLADES OF AIRCRAFT GAS TURBINE ENGINES MADE OF HEAT-RESISTANT NICKEL ALLOY ZhS32-VI

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