Reliability of Laminated Composite Beams Subjected to Subtangential Loads
Preliminary Design of a Structural Wing-Box Under a Twist Constraint
Parametric Studies of Flutter Speed in a Strut-Braced Wing
On Load Updating for Finite Element Models
Neural Networks for Inverse Problems Using Principal Component Analysis and Orthogonal Arrays
Neural Networks for Inverse Problems in Damage Identification and Optical Imaging
Effect of Compressive Force on Flutter Speed of a Strut-Braced Wing
Dynamic Stability of Laminated Composite Beams Subject to Subtangential Loads
Control Law Design in a Computational Aeroelasticity Environment
Computation of Actuation Power Requirements for Smart Wings With Morphing Airfoils
A Shear-Flexible Beam Element for Linear Analysis of Unsymmetrically Laminated Beams
AIAA-2001-1611 Effect of Compressive Force on Strut-Braced Wing Response
AIAA-2001-1295 Near-Exact Analytical Solutions to Linear Time-Variant Systems