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