A nonlinear POD reduced order model for limit cycle oscillation prediction

Science China: Physics, Mechanics and Astronomy

Volumn 53, Issue 7, 2010, Pages 1325-1332

  Chen, Gang ^a   Li, Yueming ^a   Yan, Guirong ^a  

^a XI'AN JIAOTONG UNIVERSITY   (China)

Author keywords

aeroelasticity; limit cycle oscillation; proper orthogonal decomposition; reduced order model

Indexed keywords

AEROELASTIC MODELS; AEROELASTIC SYSTEM; AIRFOIL CONFIGURATION; BACKGROUND FLOW; FLOW SOLVER; FREQUENCY DOMAINS; LIMIT CYCLE OSCILLATIONS; NON-LINEAR FLOW EQUATIONS; NONLINEAR FEATURES; PROPER ORTHOGONAL DECOMPOSITIONS; REDUCED ORDER MODELS; REDUCED-ORDER MODEL; SECOND ORDERS; SIMULATION RESULT; SMALL DISTURBANCES; TAYLOR SERIES EXPANSIONS; TIME DOMAIN;

AERODYNAMICS; AEROELASTICITY; AIRFOILS; COMPUTER SIMULATION; ELASTIC WAVES; FIGHTER AIRCRAFT; NONLINEAR EQUATIONS; TAYLOR SERIES;

OSCILLATING FLOW;

EID: 77955519257     PISSN: 16747348     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11433-010-4013-2     Document Type: Article

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