FEATURES OF THE AERODYNAMIC OPTIMIZATION OF THE SPATIAL SHAPE OF AXIAL-FLOW COMPRESSOR BLADES
This paper is concerned with the choice of rational methods for the aerodynamic improvement of blade rows of gas-turbine engines’ highly loaded axial-flow compressor stages. The paper presents an assessment of capabilities of an approach to the aerodynamic optimization of compressor blade rows devel...
Gespeichert in:
| Datum: | 2026 |
|---|---|
| Hauptverfasser: | , , |
| Format: | Artikel |
| Veröffentlicht: |
текст 3
2026
|
| Online Zugang: | https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/186 |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| Назва журналу: | Technical Mechanics |
Institution
Technical MechanicsSchreiben Sie den ersten Kommentar!