Proper orthogonal decomposition technique for the computation of nonlinear panel response

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

Volumn 1, Issue I, 2000, Pages 492-498

  Mortara, Sean A ^a   Slater, Joseph C ^a   Beran, Philip S ^a  

^a WRIGHT STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; COMPUTER SIMULATION; EIGENVALUES AND EIGENFUNCTIONS; FINITE DIFFERENCE METHOD; INTEGRAL EQUATIONS; INTEGRATION; MATHEMATICAL MODELS; MATRIX ALGEBRA; PARTIAL DIFFERENTIAL EQUATIONS; RUNGE KUTTA METHODS; STRUCTURAL PANELS; SUPERSONIC FLOW;

AERODYNAMIC PRESSURE; MACH NUMBER; NONLINEAR PANEL RESPONSE; PROPER ORTHOGONAL DECOMPOSITION METHOD;

FLUTTER (AERODYNAMICS);

EID: 0033666433     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)