Effects of uncertainty on nonlinear plate aeroelastic response

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

Volumn 1, Issue , 2002, Pages 559-568

  Lindsley, Ned J ^a   Beran, Philip S ^a   Pettit, Chris L ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTER AIDED SOFTWARE ENGINEERING; COMPUTER SIMULATION; ELASTIC MODULI; MATHEMATICAL MODELS; MONTE CARLO METHODS; OSCILLATIONS; PLATES (STRUCTURAL COMPONENTS); SUPERSONIC FLOW;

LIMIT-CYCLE OSCILLATIONS (LCO);

SUPERSONIC AERODYNAMICS;

EID: 0036072701     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-1271     Document Type: Conference Paper

References (7)

1. Influence of large amplitudes on free flexural vibrations of rectangular elastic plates
2. Piston theory - A new aerodynamic tool for the aeroelastician
3. Nonlinear oscillations of a fluttering plate
4. Prediction of nonlinear panel response using proper orthogonal decomposition