Semester : SEMESTER 7
Subject : Composite Materials
Year : 2020
Term : DECEMBER
Branch : AERONAUTICAL ENGINEERING
Scheme : 2015 Full Time
Course Code : AO 407
Page:1
D
Reg No.:
100004 0407122001 Pages: 2
Name:
APJ ABDUL KALAM TECHNOLOGICAL UNIVERSITY
Seventh Semester B.Tech Degree Examination (Regular and Supplementary), December 2020
Max. Marks: 100
1 ஐ
b)
0)
2
3 a)
b)
4
5
6
7
8
Course Code: ൧0407
Course Name: COMPOSITE MATERIALS
PARTA
Answer any three full questions, each carries 10 marks.
Differentiate between alloys and composites.
Define Strength ratio.
Give the upper limit of operating temperatures of polymer, metal, and ceramic
composites.
Define a composite material and explain the classifications of composites
according to reinforcement and matrix used.
Illustrate the variation of stress and strain in a composite laminate with suitable
diagram.
Write the Hooke’s law for isotropic Material in the form of Stiffness matrix and
compliance matrix.
Show the reduction of Anisotropic Material Stress-Strain Equation to those of
Monoclinic Stress-Strain Equation.
PART تا
Answer any three full questions, each carries 10 marks.
Derive the extensional [A], coupling [B], and bending [D] stiffness matrices for
the force and Moment Resultants Related to Mid-plane Strains and Curvatures in
a Laminates.
Compute [A] matrix for [0 / +45] laminate with the following laminate
properties. E;=14S5apa, E,=10.Sapa, 1220.28 and Gj2=7.5apa. Thickness of
each lamina is 0.25mm
Explain the different types of repair techniques used in composite materials.
Explain centrifugal casting and continuous lamination technique process of FRP
with appropriate diagram.
Page lof 2
Duration: 3 Hours
Marks
(5)
(2)
(3)
(10)
(4)
(6)
(10)
(10)
(10)
(10)
(10)