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

Proceedings of the ASME Turbo Expo

Volumn 7 B, Issue , 2013, Pages

  Krack, Malte ^a   Scheidt, Lars Panning Von ^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

COMPUTATION THEORY; DAMPING; DEGREES OF FREEDOM (MECHANICS); HARMONIC ANALYSIS; KINETICS; LARGE SCALE SYSTEMS; MODAL ANALYSIS; NONLINEAR ANALYSIS; TURBOMACHINE BLADES;

BLADED DISCS; COMPUTATIONAL EFFORT; CONTACT INTERFACE; CYCLE OSCILLATIONS; FORCED RESPONSE; LIMIT-CYCLE; NONLINEAR MODAL ANALYSIS; PRE LOADS; REDUCED ORDER MODELLING; REDUCED-ORDER MODEL;

KINETIC ENERGY;

EID: 84890166052     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/1.4025002     Document Type: Conference Paper

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