Transonic/Supersonic Aeroelastic Instability of an All Movable Wing with Structural Nonlinearity
Spectral Element Model for the Vibration of an Axially Moving Timoshenko Beam
Effect of Unsteady Blade Motion on the Aerodynamic Performance of Micro-Rotorcraft
Dynamic Analysis for Delaminated Composites Using DKQ Concept Based on Higher-Order Zig-Zag Theory
Design Optimization of Structural Acoustic Problems Using FEM-BEM
Buckling Initiation and Disbond Growth in Adhesively Bonded Composite Flanges
Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge Flaps