EisenerZ - Influence of Inflow-Nonuniformieties onto the Excitation of LPTs of Modern Two-Spool Engines

Engineering

1. Low-Pressure Turbine 100%
2. Inlet Boundary Condition 50%
3. Rotor Blade 50%
4. Simple Calculation 50%
5. Combustion Chamber 50%
6. Periodic Boundary 50%
7. Fluid-Structure Interaction 50%
8. Research Project 50%
9. Measurement Data 50%
10. Test Rig 50%
11. Boundary Condition 50%
12. Pressure Distribution 50%