Reduced order modeling based on complex nonlinear modal analysis and its application to bladed disks with shroud contact

Journal of Engineering for Gas Turbines and Power

Volumn 135, Issue 10, 2013, Pages

  Krack, Malte ^a   Panning Von Scheidt, Lars ^a   Wallaschek, Jörg ^a   Siewert, Christian ^b   Hartung, Andreas ^c  

^a LEIBNIZ UNIVERSITY HANNOVER   (Germany)

^b SIEMENS AG   (Germany)

^c MTU AERO ENGINES GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

FOURIER-GALERKIN METHODS; LIMIT CYCLE OSCILLATION (LCO); LOCALIZED NON-LINEARITIES; MULTI-HARMONIC BALANCE METHODS; NONLINEAR MODAL INTERACTIONS; NONLINEAR MODAL PROPERTIES; NUMBER OF DEGREES OF FREEDOM; ROBUST DESIGN OPTIMIZATION; BLADED DISCS; COMPUTATIONAL EFFORT; CONTACT INTERFACE; CYCLE OSCILLATIONS; FORCED RESPONSE; LIMIT-CYCLE; MODEL-BASED OPC; PRE LOADS; REDUCED ORDER MODELLING; REDUCED-ORDER MODEL;

DAMPING; FLUTTER (AERODYNAMICS); GALERKIN METHODS; KINETICS; MODAL ANALYSIS; OPTIMIZATION; AEROELASTICITY; COMPUTATION THEORY; DEGREES OF FREEDOM (MECHANICS); LARGE SCALE SYSTEMS; TURBOMACHINE BLADES;

TURBOMACHINE BLADES; KINETIC ENERGY;

EID: 84883606814     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.4025002     Document Type: Article

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