Integrated Structural Tailoring and Control Using Adaptive Materials for Advanced Aircraft Wings
Control of Cantilever Vibration via Structural Tailoring and Adaptive Materials
Vibration of Geometrically Imperfect Panels Subjected to Thermal and Mechanical Loads
Frequency-Load Interaction of Geometrically Imperfect Curved Panels Subjected to Heating
Aeroelastic response of nonlinear wing sections using a functional series techniques