Application of FDKL method for order reduction of RFA unsteady aeroelastic models

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Kim, T ^a   Nagaraja, K S ^a   Bhatia, K G ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DYNAMIC LOADS; FREQUENCY RESPONSE; RATIONAL FUNCTIONS; TIME DOMAIN ANALYSIS;

AEROELASTIC MODELING; CLOSED-LOOP ANALYSIS; CLOSED-LOOP DESIGN; COMMERCIAL AIRPLANE; ERROR MINIMIZATION; KARHUNEN-LOEVE METHOD; RATIONAL FUNCTION APPROXIMATION; REDUCED ORDER MODELS;

AEROELASTICITY;

EID: 85067319010     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1524     Document Type: Conference Paper

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