A Tool for the Design of Turbomachinery Disks for an Aero-Engine Preliminary Design Framework

Disks in gas turbines are optimized for minimum weight, while satisfying both geometry and stress constraints, in order to minimize the engine production, operation, and maintenance costs. In the present paper, a tool is described for the preliminary mechanical design of gas turbine disks. A novel f...

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Autori principali:	Ioannis Kolias, Nikolaos Aretakis, Alexios Alexiou, Konstantinos Mathioudakis
Natura:	Artigo
Lingua:	Inglês
Pubblicazione:	MDPI AG 2023-05-01
Serie:	Aerospace
Soggetti:	gas turbines preliminary design mechanical design rotating disks thermal analysis stress analysis
Accesso online:	https://www.mdpi.com/2226-4310/10/5/460
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