H2-TCF - Aerothermale Untersuchung eines aggressiven Turbinenzwischengehäuses im neuen Spannungsfeld der Wasserstoffverbrennung

Engineering

1. Intermediate Casing 100%
2. Stress Field 100%
3. Turbine Inlet Temperature 100%
4. Test Campaign 50%
5. Combustion Chamber 50%
6. Computational Fluid Dynamics 50%
7. High-Pressure Turbine 50%
8. Internals 50%
9. Combustor 50%
10. Deep Understanding 50%
11. Cooling Effect 50%
12. Test Rig 50%
13. Flow Phenomenon 50%
14. Inlet Temperature 50%
15. Maximum Temperature 50%
16. Aero-Engines 50%