Some aspects of wake-wake interactions regarding turbine stator clocking

Journal of Turbomachinery

Volumn 123, Issue 3, 2001, Pages 526-533

  Tiedemann, M ^a   Kost, F ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

HIGH PRESSURE EFFECTS; NOZZLES; ROTORS; STREAM FLOW; TURBINES; TURBULENCE;

NOZZLE GUIDE VANE (NGV);

STATORS;

INTERACTION; PRESSURE DISTRIBUTION; STATOR; TURBOMACHINERY; UNSTEADY FLOW; WAKE;

EID: 0035389129     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1370158     Document Type: Article

References (19)

1. Blade row interaction in a multistage low-pressure turbine
2. Effects of stator indexing on performance in a low speed multistage axial compressor
3. Experimental and numerical investigation of airfoil clocking and inter-blade-row gap effects on axial compressor performance
4. Full-Annulus simulations of airfoil clocking in a 1-1/2 stage axial compressor
5. Physics of airfoil clocking in axial compressors
6. Physics of airfoil clocking in a high speed axial compressor
7. Unsteady flows in turbines-impact on design procedure
8. Performance improvement through indexing of turbine airfoils: Part 1-Experimental investigation
9. Performance improvement through indexing of turbine airfoils: Part 2-Numerical simulation
10. "Boundary layer development in axial compressors and turbines," Part 1 of 4-Composite picture
11. Numerical investigations of the clocking effects in a multistage turbine
12. A study of turbine performance increases through airfoil clocking
13. The effects of turbulence and stator/rotor interactions on turbine heat transfer, Part I-Design operating conditions
14. Turbine blade unsteady heat transfer change due to stator indexing
15. Reduction of unsteady blade loading by beneficial use of vortical and potential disturbances in an axial compressor with rotor clocking
16. The influence of wake-wake interactions on loss fluctuations of a downstream axial compressor blade row
17. Application of laser-two-focus vorlocimetry to transonic turbine flows
18. Stator wake effects on the total pressure distribution downstream of a transonic turbine rotor
19. Unsteady boundary layer transition on a high pressure turbine rotor blade