Limit cycle oscillation prediction and control design method for aeroelastic system based on new nonlinear reduced order model

International Journal of Computational Methods

Volumn 8, Issue 1, 2011, Pages 77-90

  Chen, Gang ^a   Li, Yue Ming ^a   Yan, Gui Rong ^a  

^a XI'AN JIAOTONG UNIVERSITY   (China)

Author keywords

active control; aeroelasticity; limit cycle oscillation; proper orthogonal decomposition; Reduced order model

Indexed keywords

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

AERODYNAMICS; AEROELASTICITY; CONTROL THEORY; DELTA SIGMA MODULATION; DESIGN; ELASTIC WAVES; NONLINEAR EQUATIONS; PRINCIPAL COMPONENT ANALYSIS; TAYLOR SERIES; TIME DOMAIN ANALYSIS;

OSCILLATING FLOW;

EID: 79952612345     PISSN: 02198762     EISSN: None     Source Type: Journal    
DOI: 10.1142/S0219876211002435     Document Type: Article

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