| Ref.No: | 62427100 |
| Start date: | 03.07.2024 |
| End date: | 02.12.2025 |
| Approval date: | 19.06.2024 |
| Department: | MECHANICAL ENGINEERING |
| Sector: | FLUIDS |
| Financier: | SAFRAN AIRCRAFT ENGINES |
| Budget: | 74.400,00 € |
| Public key: | Ψ59Φ46ΨΖΣ4-ΔΛΓ |
| Scientific Responsible: | Prof. MATHIOUDAKIS |
| Email: | kmathiou@central.ntua.gr |
| Description: | THE PURPOSE OF THE WORK L IS TO DEMONSTRATE THE USE OF A COMPRESSOR MEAN-LINE MODEL, FOR GENERATING A COMPLETE PERFORMANCE MAP, WHERE THE CORRELATIONS FOR LOSSES AND DEVIATION ANGLES ARE REPLACED BY CORRESPONDING SURROGATE MODELS, DERIVED FROM HIGHER-FIDELITY TOOLS AND KNOWN PHYSICAL BEHAVIOUR. A THREE-STEP APPROACH WILL BE FOLLOWED STARTING WITH THE HIGH-FIDELITY CALCULATIONS, FOLLOWED BY THE GENERATION OF THE APPROPRIATE SURROGATE MODELS AND FINALLY THEIR IMPLEMENTATION IN THE MEAN-LINE CODE. |
