A fast aeroelastic response prediction method based on proper orthogonal decomposition reduced order model

Yuhang Xuebao/Journal of Astronautics

Volumn 30, Issue 5, 2009, Pages

  Chen, Gang ^a   Li, Yue Ming ^a   Yan, Gui Rong ^a   Xu, Min ^b   Zeng, Xian Ang ^b  

^a XI'AN JIAOTONG UNIVERSITY   (China)

^b NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Balanced truncation; Computational aeroelasticiy; Proper orthogonal decomposition; Reduced order model

Indexed keywords

AEROELASTIC DYNAMIC RESPONSE; AEROELASTIC RESPONSE; AEROELASTIC SYSTEM; BALANCED TRUNCATION; BALANCED TRUNCATION METHOD; CFD/CSD; COMPUTATION EFFICIENCY; COUPLED METHOD; COUPLED NUMERICAL SIMULATION; FLUTTER BOUNDARIES; FREQUENCY DOMAINS; HIGHER ORDER; IN-CONTROL; NUMERICAL RESULTS; ORDER OF MAGNITUDE; PROPER ORTHOGONAL DECOMPOSITIONS; REDUCED ORDER MODELS; TIME DOMAIN;

COMPUTATIONAL EFFICIENCY; COMPUTER SIMULATION; DYNAMIC RESPONSE; NUMERICAL ANALYSIS;

TIME DOMAIN ANALYSIS;

EID: 70350365921     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: 10.3873/j.issn.1000-1328.2009.05.004     Document Type: Article

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