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+keyword:(spacecraft structures)
Reliability of Laminated Composite Beams Subjected to Subtangential Loads
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
Computational Model for Progressive Failure of Adhesively Bonded Joints
Preliminary Design of a Structural Wing-Box Under a Twist Constraint
Control Law Design in a Computational Aeroelasticity Environment