Flutter mechanism in low pressure turbine blades

Journal of Engineering for Gas Turbines and Power

Volumn 122, Issue 1, 2000, Pages 82-88

  Nowinski M , Panovsky J ^a  

^a EPFL   (Switzerland)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; FLUTTER (AERODYNAMICS);

STABLIZING EFFECT;

GAS TURBINES;

AIRCRAFT; BLADE; FLUTTER; LOW PRESSURE; TURBINE;

EID: 0033812197     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.483179     Document Type: Article

References (17)

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3. Aerodynamic superposition principle in vibrating turbine cascades
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6. Aeroelastic formulation for tuned and mistuned rotors
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9. Flutter and response of a mistuned cascade in incompressible flow
10. Steady-state and time-dependent experimental results of a NACA-3506 cascade in an annular channel
11. System mode shapes in the flutter of compressor blade rows
12. Flutter of aircraft engine low pressure turbine blades
13. A design method to prevent low pressure turbine blade flutter
14. The spacing of turbomachinery blading, especially with large angular deflection