The functional advantages of tailored stiffness, often seen in nature, are also utilized in
composite structures. Advancements in the multiaxis tow placement and automated fiber …

Aeroelastic optimization has become an indispensable component in the evaluation of
divergence and flutter characteristics for plated/shell structures. The present paper intends to …

In this paper, thermal buckling analysis of variable stiffness composite laminate (VSCL) is
carried out. The first-order shear deformation theory is adopted with eight noded …

This work focuses on the layerwise finite element modelling and active aeroelastic flutter
control of smart variable stiffness laminated composite panels with surface bonded …

In this work, an assessment of layerwise finite element models for supersonic flutter analysis
of soft core viscoelastic sandwich panels is presented, making use of various kinematic …

This article addresses a study about the dynamic crack propagation in Variable Stiffness
Composite Laminates (VSCLs) under non-classic thermal shock considering Lord …

This paper addresses the influence of material and fabrication uncertainties on natural
frequencies of curvilinear fiber laminate. Material properties and fiber orientation are …

Compared to straight fiber path laminates, variable-angle tow (VAT) laminates are known to
redistribute the in-plane stress resultants for improving structural buckling response. The …

This work focuses on panel flutter and active control in supersonic variable stiffness
composite laminates, making progress on the analytical modeling and combined exploration …

Aeroelastic stability of tapered/skew variable stiffness composite cantilevered plates are
considered in the current study at flutter and post-flutter regions. The variable stiffness …