Experimental and numerical investigation of rotating bladed disk forced response using underplatform friction dampers

Journal of Engineering for Gas Turbines and Power

Volumn 130, Issue 4, 2008, Pages

  Sever, Ibrahim A ^a   Petrov, Evgeny P ^b   Ewins, David J ^b  

^a ROLLS ROYCE PLC   (United Kingdom)

^b IMPERIAL COLLEGE LONDON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

DISKS (STRUCTURAL COMPONENTS); EXPERIMENTS; FRICTION; GAS DYNAMICS; ROTATING DISKS; ROTATION; TURBOMACHINE BLADES;

AERODYNAMIC EFFECTS; BLADED DISKS; DEGREE OF CORRELATIONS; EXPERIMENTAL DATA; EXPERIMENTAL INVESTIGATIONS; FORCED RESPONSES; FORCED VIBRATIONS; FRICTION DAMPERS; IMPERIAL COLLEGE; MEASURED DATA; MEASUREMENT TECHNIQUES; MISTUNING; NON-CONTACT; NUMERICAL INVESTIGATIONS; NUMERICAL PREDICTIONS; PRECISE MEASUREMENTS; PREDICTION TOOLS; RESPONSE CURVES; TEST RIGS;

FORECASTING;

EID: 53649110271     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2903845     Document Type: Article

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