A numerical control design method for prototypical aeroelastic wing section with structural non-linearity.
Péter BaranyiRon J. PattonPublished in: ECC (2003)
Keyphrases
- theoretical analysis
- high accuracy
- significant improvement
- computational cost
- segmentation method
- detection method
- sensitivity analysis
- experimental evaluation
- high precision
- classification accuracy
- pairwise
- multiscale
- optimization method
- structural information
- fully automatic
- data sets
- partial differential equations
- classification method
- synthetic data
- prior knowledge
- similarity measure
- learning algorithm
- neural network