Title of article :
Experimental and Numerical Free Vibration Analysis of Hybrid Stiffened Fiber Metal Laminated Circular Cylindrical Shell
Author/Authors :
Nazari, A Department of Aerospace Engineering - Aerospace Research Institute, Tehran , Malekzadeh, K Malek Ashtar University, Tehran , Naderi, A.A Faculty of Mechanical Engineering - Emam Ali University, Tehran
Abstract :
The modal testing has proven to be an effective and non-destructive test
method for estimation of the dynamic stiffness and damping constant.
The aim of the present paper is to investigate the modal response of
stiffened Fiber Metal Laminated (FML) circular cylindrical shells using
experimental and numerical techniques. For this purpose, three types of
FML-stiffened shells are fabricated by a specially-designed method and
the burning examination is used to determine the mechanical properties
of them. Then, modal tests are conducted to investigate the vibration and
damping characteristics of the FML-stiffened shells. A 3D finite element
model is built using ABAQUS software to predict the modal
characteristics of the FML-stiffened circular cylindrical shells with freefree
ends. Finally, the achievements from the numerical and experimental
analyses are compared with each other and good agreement has been
obtained. Modal analyses of the FML-stiffened circular cylindrical shells
are investigated for the first time in this paper. Thus, the results obtained
from this study are novel and can be used as a benchmark for further
studies.
Keywords :
Free vibration , FML-stiffened shell , Modal test , Experimental study
Journal title :
Astroparticle Physics