Prediction of the resonant response of frictionally constrained blade systems using constrained mode shapes

Proceedings of the ASME Turbo Expo

Volumn 5, Issue , 1998, Pages

  Chen, J J ^a   Menq, C H ^a  

^a The Ohio State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; CUTTING EQUIPMENT; FINITE ELEMENT METHOD; FORECASTING; FRICTION; TRIBOLOGY;

ACCURATE PREDICTION; BLADE SYSTEMS; CYCLIC SYMMETRY; FRICTION CONTACT; RESONANT RESPONSE; SHROUDED BLADES; SINGLE BLADES; VIBRATION MODES;

GAS TURBINES;

EID: 84973100835     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/98-GT-548     Document Type: Conference Paper

References (14)

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