This document discusses modeling the elastic properties of laminated composites. It first defines composites as materials made of two or more distinct constituent materials. It then discusses various properties of composites like strength and corrosion resistance. It classifies composites based on their matrix material and reinforcement type. It also discusses volume and weight fractions. Rules of mixture are presented for calculating longitudinal and transverse modulus. Stress-strain relationships and analysis methods for orthotropic laminates are described. Forces, moments, and the inverse of the stiffness matrix for laminated composites are defined. Computer simulation of composite modeling allows for virtual testing of multiple design scenarios.
Image result for metal matrix composites
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A metal matrix composite (MMC) is composite material with at least two constituent parts, one being a metal necessarily, the other material may be a different metal or another material, such as a ceramic or organic compound. When at least three materials are present, it is called a hybrid composite.
Composite Materials are widely used in day today life and as well as in automotive and aerospace industry which are monolithic composites.but most of the monolithic composites are not able to achieve required mechanical properties,so to achieve those mechanical properties Metal Matrix composites widely used in different sectors.some of Compiled information on MMC are presented in this presentation.
Image result for metal matrix composites
www.slideshare.net
A metal matrix composite (MMC) is composite material with at least two constituent parts, one being a metal necessarily, the other material may be a different metal or another material, such as a ceramic or organic compound. When at least three materials are present, it is called a hybrid composite.
Composite Materials are widely used in day today life and as well as in automotive and aerospace industry which are monolithic composites.but most of the monolithic composites are not able to achieve required mechanical properties,so to achieve those mechanical properties Metal Matrix composites widely used in different sectors.some of Compiled information on MMC are presented in this presentation.
Fracture and failure analyses of plastics and reinforced plasticsPadmanabhan Krishnan
This ppt describes the structure property correlationship between structure, microstructure and the observed properties of plastics and reinforced plastics./ Fracture , failure analysis and fractography are discussed in details.
Fracture and failure analyses of plastics and reinforced plasticsPadmanabhan Krishnan
This ppt describes the structure property correlationship between structure, microstructure and the observed properties of plastics and reinforced plastics./ Fracture , failure analysis and fractography are discussed in details.
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various combinations of end conditions is studied. To verify the accuracy of the present method, the frequency
parameters are evaluated and compared with previous work available in the literature. The good agreement with
other available data demonstrates the capability and reliability of the finite element method and the adopted beam
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Effect of lamination angle on maximum deflection of simply supported composit...RAVI KUMAR
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The main objective of the paper is to find out the lamination angle at which minimum deflection is obtained & to find out the effect of lamination angle on maximum transverse deflection of the beam.
Analysis of Cross-ply Laminate composite under UD load based on CLPT by Ansys...IJERA Editor
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orthotropic properties. The loading in current study is supposed to be of uniformly distributed load type. For the
analysis purpose software working on finite element analysis logics i.e. Ansys mechanical APDL is used. By the
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laminate layers is also studied in current study along with the effect of variation of stacking patterns. The current
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International Journal of Engineering Research and DevelopmentIJERD Editor
Electrical, Electronics and Computer Engineering,
Information Engineering and Technology,
Mechanical, Industrial and Manufacturing Engineering,
Automation and Mechatronics Engineering,
Material and Chemical Engineering,
Civil and Architecture Engineering,
Biotechnology and Bio Engineering,
Environmental Engineering,
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Aerospace Engineering.
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About
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Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
Key Features
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface
• Compatible with MAFI CCR system
• Copatiable with IDM8000 CCR
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
Application
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
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1. “Modeling of elastic properties
of laminates”
By: Harsh Kumar
18ME4109
Machine Design
National Institute Of Technology Durgapur
2. Composites
The word “composites” means “consisting of two or more distinct parts”. Thus a material
having two or more distinct constituent materials or phases may be considered a composite
material.
3. Properties of composites
Properties of composites are strongly influenced by the properties of their constituent materials,
their distribution, and the interaction among them. The composite properties may be the volume
fraction sum of the properties of the constituents.
Its various properties are:
1) LIGHT WEIGHT
2) HIGH STRENGTH
3) STRENGTH RELATED TO WEIGHT
4) CORROSION RESISTANCE
5) HIGH-IMPACT STRENGTH
6) DESIGN FLEXIBILITY
7) DIMENSIONAL STABILITY
8) NONCONDUCTIVE
9) NONMAGNETIC
10)DURABLE
11)LOW THERMAL CONDUCTIVITY
4. Classification of composites
On the basis of matrix
material
Polymer
Matrix
Thermosets
Thermoplastic
Ceramic
matrix
Metal matrix
6. Volume and weight fraction
Volume fraction and weight fraction are denoted by capital letters V and W respectively.
Subscript m, f and c are used to represent matrix, fiber, composite respectively.
Let
vc = volume of composite and wc = weight of composite
vf = volume of fiber and wf = weight of fiber
vm = volume of matrix and wc = weight of matrix
then volume fraction and weight fraction are given by
7. Rule of mixture
The upper bound on the composite modulus E according to rule of mixture is given by the
following relation and will represent longitudinal modulus of elasticity EL
EL=Ef*Vf+Em*Vm
8. The lower bound on the composite modulus E according to rule of mixture is given by the
following relation and will represent transverse modulus of elasticity ET
1
𝐸 𝑇
=
𝑉 𝑓
𝐸 𝑓
+
𝑉 𝑚
𝐸 𝑚
Shear modulus:
Poisson’s ratio:
9. Analysis of an orthotropic laminates
A single layer of laminated composite material is referred
as lamina. Several laminae are bonded together to form a
structure termed as laminate. Orientation of laminae are
chosen to meet laminate design requirement. Orthotropic
material, whose behavior lies between isotropic and
anisotropic material.
16. Analysis of orthotropic laminated composite:
Bond between two laminae is assumed to be perfect. i.e. infinitesimely
thin, not shear deformable, no slip between layer, displacement remain
continuous across the bond
Stress strain relationship:
u0
w0x
z
B
C
A
B’
17. Forces and moment in lamina:
x
y
x
y
z Nx
Ny
Nxy
Nyx
Mx
My
MxyMyx
Force in lamina
Moment in lamina
Where h = thickness of lamina
18. Forces in orthotropic laminated composite:
h
1
2
n
k
h0
h1
h2
hn
hn-1
hk-1
hk
Mid plane
Geometry of laminate
20. in short,
where A: extensional stiffness matrix
B: bending-extension coupling stiffness matrix
D: bending stiffness matrix
Combining both force and moment equation together, it can be written as:
(1)
21. However, in most experiments, loads are applied and the resulting deformations are
measured, i.e. the deformations are the dependent variables, not the loads. Thus the
expressions for the middle surface extensional strains and curvatures in terms for force and
moment resultants would be convenient.
The first step in the derivation of inverse of equation (1) is to write it in the form
(2)
(3)
and solve for Equation (2) for ℇ0
ℇ0
= 𝐴−1
N - 𝐴−1
Bk (4)
whereupon Equation (3) becomes
M= B𝐴−1N + (-B 𝐴−1B+D)k (5)
Equation (4) and (5) can be written as
(6)
22. or, ℇ0 = A*N + B*k (7)
M = H*N + D*k (8)
where B* is not equal to H*. Now solve Equation (8) for k.
k = 𝐷∗−1
M − 𝐷∗−1
H∗N (9)
and substitute in Equation (7) to get
ℇ0 = B* 𝐷∗−1M + (A* - B* 𝐷∗−1H*)N (10)
Thus,
(11)
or
Now we can calculate stress in each lamina by using following relation
24. Conclusion
To reduce the amount of prototype testing – Computer
simulation allows multiple “what-if” scenarios to be tested
quickly and effectively.
It is cost saving, time saving and creates more reliable better
quality designs.