Abstract
The free vibration responses of the hybrid composites curved panel have been investigated in the present work. The hybrid composite is modelled numerically using the first-order shear deformation theory (FSDT). The finite element method is utilized via ANSYS and the responses are computed using a parametric design language (APDL) code. The correctness and performance of the present model has been proved and authenticated by comparing the presently calculated values with published results. Finally, the influence of shell panel geometry, constraint conditions, curvature ratio and types of hybrid on the modal behavior of the hybrid composite curved panel have been discussed in detail.
Sign-in/Register to access full text options 
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
