Event Title

Analysis of Laminated Composite Plate Under Combined Loads at Various Lamination Angles

Presenter Information

Divya Sree AnusuriFollow

Faculty Mentor

Dr. Tahsin Khajah

Document Type

Oral Presentation

Date of Publication

April 2021

Abstract

In this paper, analysis is performed to predict engineering properties of multilayered plate, effects of moisture and temperature and the stress-strain distributions for various lamination angles of continuous fiber composite laminate is described. Plane classical lamination theory and stress-strain relationships are mainly used for analysis. The analyzed laminate plates have been composed with unidirectional layers that were made from composite materials: the reinforcement fibers were E-glass and as matrix material the epoxy resin were used. The engineering properties values of multilayered plate and several of the numerous results of the stress-strain distributions in the layers of the analyzed laminated plate subjected to known the force resultant Nx and bending moment resultant Mx graphically in diagrams are presented. The numerical results in this work were calculated using MATLAB software.

Keywords

Laminated composite material, elastic properties, stress

Persistent Identifier

http://hdl.handle.net/10950/3119

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Apr 16th, 11:00 AM Apr 16th, 12:00 PM

Analysis of Laminated Composite Plate Under Combined Loads at Various Lamination Angles

In this paper, analysis is performed to predict engineering properties of multilayered plate, effects of moisture and temperature and the stress-strain distributions for various lamination angles of continuous fiber composite laminate is described. Plane classical lamination theory and stress-strain relationships are mainly used for analysis. The analyzed laminate plates have been composed with unidirectional layers that were made from composite materials: the reinforcement fibers were E-glass and as matrix material the epoxy resin were used. The engineering properties values of multilayered plate and several of the numerous results of the stress-strain distributions in the layers of the analyzed laminated plate subjected to known the force resultant Nx and bending moment resultant Mx graphically in diagrams are presented. The numerical results in this work were calculated using MATLAB software.