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