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

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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Bibliographic Details
Main Authors: Ioannis Kolias, Nikolaos Aretakis, Alexios Alexiou, Konstantinos Mathioudakis
Format: Article
Language:English
Published: MDPI AG 2023-05-01
Series:Aerospace
Subjects:
gas turbines
preliminary design
mechanical design
rotating disks
thermal analysis
stress analysis
Online Access:https://www.mdpi.com/2226-4310/10/5/460

Internet

https://www.mdpi.com/2226-4310/10/5/460

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