An optimal reduced-order aeroelastic modeling based on a response-based modal analysis of unsteady CFD models

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 2001, Pages 2544-2554

  Kim, T ^a   Bussoletti, J E ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; COMPUTATIONAL FLUID DYNAMICS; EIGENVALUES AND EIGENFUNCTIONS; FREQUENCY DOMAIN ANALYSIS; GALERKIN METHODS; MATHEMATICAL MODELS; MODAL ANALYSIS; OPTIMIZATION; STRUCTURAL ANALYSIS; TIME DOMAIN ANALYSIS;

AEROELASTIC MODELING; EIGENFORMULATION; KARHUEN LOEVE MODES; MODEL REDUCTION TECHNIQUE; STRUCTURAL MODEL;

AERODYNAMICS;

EID: 0035006811     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)