AIAA-2001-1611 Effect of Compressive Force on Strut-Braced Wing Response
AIAA-2001-1295 Near-Exact Analytical Solutions to Linear Time-Variant Systems
Influence of External Store Aerodynamics on Flutter/LCO of a Fighter Aircraft
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
Nonlinear Response of Open/Closed-Loop Aeroelastic System Using a Discrete State-Space Approach
Reliability of Laminated Composite Beams Subjected to Subtangential Loads
Dynamic Stability of Laminated Composite Beams Subject to Subtangential Loads
Neural Networks for Inverse Problems Using Principal Component Analysis and Orthogonal Arrays
Body-Flexure Control with Smart Actuation for Hypervelocity Missiles
Effect of Compressive Force on Flutter Speed of a Strut-Braced Wing
Preliminary Design of a Structural Wing-Box Under a Twist Constraint
Control Law Design in a Computational Aeroelasticity Environment