Sensitivity of tuned bladed disk response to frequency veering

Journal of Engineering for Gas Turbines and Power

Volumn 127, Issue 4, 2005, Pages 835-842

  Kenyon, James A ^a   Griffin, J H ^b   Kim, N E ^c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b CARNEGIE MELLON UNIVERSITY   (United States)

^c Hood Technology Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; EIGENVALUES AND EIGENFUNCTIONS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; NATURAL FREQUENCIES; NUMERICAL METHODS; ROTORS; SENSITIVITY ANALYSIS; STIFFNESS MATRIX; TURBOMACHINE BLADES; VIBRATIONS (MECHANICAL);

CYCLIC SYMMETRY MODES; FREQUENCY VEERING; TUNED BLADED DISK;

DISKS (MACHINE COMPONENTS);

MODELING;

EID: 27144521604     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1924486     Document Type: Article

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