Experimental demonstration of maximum mistuned bladed disk forced response

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 4, Issue , 2003, Pages 195-205

  Kenyon, J A ^a   Griffin, J H ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b CARNEGIE MELLON UNIVERSITY   (United States)

Author keywords

Blade vibration; Experiment; Forced response; Maximum response; Mistuning

Indexed keywords

BLADE VIBRATIONS; TRAVELING WAVES;

COMPUTER SIMULATION; FATIGUE OF MATERIALS; NATURAL FREQUENCIES; STRUCTURAL ANALYSIS; TURBINES; VIBRATIONS (MECHANICAL);

TURBOMACHINE BLADES;

EID: 0347596572     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38060     Document Type: Conference Paper

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