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...
I tiakina i:
| Ngā kaituhi matua: | , , , |
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| Hōputu: | Artigo |
| Reo: | Inglês |
| I whakaputaina: |
MDPI AG
2023-05-01
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| Rangatū: | Aerospace |
| Ngā marau: | |
| Urunga tuihono: | https://www.mdpi.com/2226-4310/10/5/460 |
| Ngā Tūtohu: |
Kāore He Tūtohu, Me noho koe te mea tuatahi ki te tūtohu i tēnei pūkete!
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