Reliability of Laminated Composite Beams Subjected to Subtangential Loads
Preliminary Design of a Structural Wing-Box Under a Twist Constraint
Neural Networks for Inverse Problems Using Principal Component Analysis and Orthogonal Arrays
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