Flow interaction from the exit cavity of an axial turbine blade row labyrinth seal

Journal of Turbomachinery

Volumn 123, Issue 2, 2001, Pages 342-352

  Pfau, A ^a   Treiber, M ^a   Sell, M ^a   Gyarmathy, G ^a  

^a ETH ZURICH   (Switzerland)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS; LEAKAGE (FLUID); TURBOMACHINE BLADES;

LABYRINTH CAVITY FLOW;

STEAM TURBINES;

AXIAL FLOW; LABYRINTH SEAL; ROTOR; TURBINE;

EID: 0035299163     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1368124     Document Type: Article

References (21)

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4. Tip clearance affected flow fields in a turbine blade row
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6. Flow visualization and leakage measurements of stepped labyrinth seals; Part I: Annular groove
7. An experimental study on labyrinth seals for steam turbines
8. Performance of worn labyrinth seals
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13. Einfluss der Kammerströmung auf die Kräfte im endlich langen Spalt einer Labyrinthdichtung
14. An experimental study of the tip leakage flow around shrouded turbine blades
15. Data acquisition and control within the Zürich annular cascade
16. The design and construction of a new test stand for the study of basic turbine flow phenomena
17. A fuzzy logic controller to balance pneumatic multi-hole probes
18. Analysis of error propagation arising from measurements with a miniature 5-hole probe