Flutter of low pressure turbine blades with cyclic symmetric modes: A preliminary design method

Journal of Turbomachinery

Volumn 126, Issue 2, 2004, Pages 306-309

  Kielb, Robert ^a   Barter, Jack ^b   Chernycheva, Olga ^c   Fransson, Torsten ^c  

^a DUKE UNIVERSITY   (United States)

^b GE AVIATION   (United States)

^c ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; MACHINE DESIGN; PRESSURE MEASUREMENT; TURBOMACHINE BLADES;

AERODYNAMIC ANALYSIS; LOW PRESSURE TURBINE (LPT); SYMMETRIC NODES; TIP SHROUD; TRANSLATIONS;

TURBINES;

DESIGN;

EID: 7644240956     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1650380     Document Type: Article

References (2)

1. Panovsky, J., and Kielb, R. E., 1998, "A Design Method to Prevent Low Pressure Turbine Blade Flutter," ASME Paper No. 98-GT-575.
2. Tchernycheva, O. V., Fransson, T. H., Kielb, R. E., and Barter, J., 2001, "Comparative Analysis of Blade Mode Shape Influence on Flutter of Two-Dimensional Turbine Blades," ISABE-2001-1243, XV ISOABE Conference, Sept. 2-7, Bangalore, India.