ENOVAL - Untersuchung eines beschaufelten Zwischendiffusors mit und ohne HDT-Rotor

Engineering

1. Engine 100%
2. Module 100%
3. Pressure System 50%
4. Fan 50%
5. Pressure Ratio 50%
6. Significant Reduction 50%
7. Aero-Engines 50%
8. Low Pressure 50%
9. Propulsion System 50%