The aim of this paper is to propose a methodology for identifying the pressure field applied on laminated composite plate from its measured vibration response. general framework study Corrected Force Analysis Technique (CFAT), which was previously used isotropic plates. This method estimates spatial derivatives equation motion with finite difference scheme and corrects bias error generated by a...

A mathematical model for enhancing the torsional stability of a slender, tapered, composite wind turbine blade is presented. The increase of the stability boundary is measured by maximization of the critical wind speed at which failure may occur by aeroelastic divergence in parked-turbine state. The total structural mass of the blade is kept constant in order not to violate other economic and p...