Abstract
Sheet shaping at optimal temperature is considered. Three methods of producing aircraft fairings are simulated. The equipment required is discussed. Conclusions are reached regarding the industrial shaping of components.
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Translated by B. Gilbert
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Kovalevich, M.V., Goncharov, A.V. Isothermal Stamping of Aluminum- and Titanium-Alloy Sheet. Russ. Engin. Res. 41, 172–174 (2021). https://doi.org/10.3103/S1068798X21020106
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DOI: https://doi.org/10.3103/S1068798X21020106