Aeroelastic system development using proper orthogonal decomposition and Volterra theory

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  Lucia, David J ^a   Beran, Philip S ^a   Silva, Walter A ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC MODELING; HYBRID METHODOLOGIES; IMPLICIT INTEGRATION; LIMIT CYCLE OSCILLATIONS; ORDERS OF MAGNITUDE; PROPER ORTHOGONAL DECOMPOSITIONS; REDUCED ORDER MODELS; SUPERSONIC CROSS FLOW;

INITIAL VALUE PROBLEMS; PRINCIPAL COMPONENT ANALYSIS; RESEARCH; STATE SPACE METHODS; STRUCTURAL DYNAMICS;

AEROELASTICITY;

EID: 84896884399     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (30)

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