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...
Enregistré dans:
| Auteurs principaux: | , , , |
|---|---|
| Format: | Artigo |
| Langue: | Inglês |
| Publié: |
MDPI AG
2023-05-01
|
| Collection: | Aerospace |
| Sujets: | |
| Accès en ligne: | https://www.mdpi.com/2226-4310/10/5/460 |
| Tags: |
Pas de tags, Soyez le premier à ajouter un tag!
|