POD-based aeroelastic analysis of a complete F-16 configuration: ROM adaptation and demonstration

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

Volumn 9, Issue , 2005, Pages 6103-6118

  Lieu, Thuan ^a,c   Farhat, Charbel ^a,c   Lesoinne, Michel ^b,d  

^a STANFORD UNIVERSITY   (United States)

^b UNIVERSITY OF COLORADO   (United States)

^c Stanford University   (United States)

^d UCB 450   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FLUTTER (AERODYNAMICS); INTERPOLATION; MATHEMATICAL MODELS; PROBLEM SOLVING;

AEROELASTIC FREQUENCIES; MACH NUMBER; PROPER ORTHOGONAL DECOMPOSITION METHOD (POD);

AERODYNAMICS;

EID: 28844480981     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2295     Document Type: Conference Paper

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