RANDOM VIBRATION ANALYSIS OF SANDWICH COMPOSITE BEAMS

Abstract

 In this thesis, a sandwich composite for Semi-monocoque construction in aircraft fuselage is analyzed for its strength under different loading conditions using different materials for Stringers balsa wood, syntactic foams, and honeycombs and Carbon Fiber reinforced thermoplastics is used as skin material. 3D modeling is done in Pro/Engineer. Static, Modal and Random Vibration analysis is done on the beam using finite element analysis software Ansys.

Authors and Affiliations

K. Ravindranath Tagore

Keywords

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  • EP ID EP107253
  • DOI 10.5281/zenodo.155243
  • Views 70
  • Downloads 0

How To Cite

K. Ravindranath Tagore (30).  RANDOM VIBRATION ANALYSIS OF SANDWICH COMPOSITE BEAMS. International Journal of Engineering Sciences & Research Technology, 5(9), 769-779. https://europub.co.uk/articles/-A-107253