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A sensitivity analysis of linear and nonlinear elastic and viscoelastic panel responses
Harry H. Hilton
National Center for Supercomputing Applications (NCSA)
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Keyphrases
Numerical Simulation
100%
Linear Relation
100%
Nonlinear Elasticity
100%
Linear Elastic
100%
Structural Materials
100%
Servo Control
100%
Nonlinear Viscoelastic Material
100%
Inertia
100%
Aerodynamics
100%
Analytical Sensitivity
100%
Sensitivity Analysis
100%
Structural Control
100%
Dynamic Relation
100%
Phase Relations
100%
Linear Solution
100%
UAV
100%
Panel Response
100%
Nonlinear Relation
100%
Lifting Surface
100%
Aerodynamic Noise
100%
Aerodynamic Loads
100%
Flight Vehicle
100%
Aero
100%
Panel Flutter
100%
Elastic Panel
100%
Viscoelastic Panel
100%
Panel Buckling
100%
Sensitivity Comparison
100%
Engineering
Unmanned Aerial Vehicle
100%
Buckling
100%
Computer Simulation
100%
Full Scale
100%
Piezoelectric
100%
Servo Control
100%
Structural Materials
100%
Panel Response
100%
Aerodynamic Noise
100%
Lifting Surface
100%
Individual Term
100%
Aerodynamic Load
100%