This document provides information about the AE-681 Composite Materials course taught by Dr. PM Mohite. The course covers topics such as introduction to unidirectional composites, analysis of lamina using classical laminate theory, design considerations, micromechanics, and performance under adverse environments. Reference materials include textbooks on composite materials and research papers. Students will be evaluated based on midterm exams, assignments, and a final exam. Attendance will be monitored and late or copied assignments will be penalized.
This document discusses mechanical properties that can be determined from tensile and shear tests. It defines key terms like stress, strain, elastic modulus, yield strength, and tensile strength. A typical stress-strain curve is shown and each region is explained. The elastic portion is linear up to the yield point, then the plastic region involves necking and strain hardening until ultimate failure. True stress and strain account for changes in cross-sectional area during deformation. The document also compares properties like ductility and toughness between different materials.
This document summarizes a student project that studied the mechanical behavior of an aluminum alloy reinforced with alumina and rice husk ash particles. Key points:
- Aluminum alloy 6061 was reinforced with 2% and 4% weight additions of alumina and rice husk ash particles via stir casting.
- Testing showed that the reinforced composites had higher ultimate tensile strength, hardness, flexural strength, and density compared to the unreinforced alloy.
- Microstructural analysis using SEM confirmed good dispersion and retention of the alumina and rice husk ash reinforcement particles in the aluminum matrix.
The document summarizes composites and their classification. It discusses that composites are made of two or more materials to produce new properties. Composites are classified based on the matrix and reinforcement geometry. The main matrix types are polymer, metal, ceramic. Reinforcements include fibers, sheets and particles. Fiber reinforced composites are widely used. Applications of composites include aerospace, automotive, construction, medical and more due to their high strength and stiffness but low density.
Griffith proposed that brittle materials contain fine cracks that concentrate stress below the theoretical strength, causing fracture. When a crack propagates, the new surface area requires energy from the released elastic strain energy of the material. Griffith established that a crack will propagate when the decrease in elastic strain energy is equal to or greater than the energy required to create the new surface. The stress intensity factor describes the stress near a crack tip and is used to predict crack propagation. Fracture toughness is the material property describing a material's resistance to crack propagation.
This document summarizes a seminar presentation on ceramic matrix composites (CMCs). CMCs consist of a ceramic matrix with reinforcements. They offer advantages over monolithic ceramics like higher toughness, strength, and fatigue resistance. Some key applications of CMCs mentioned are in cutting tools, aerospace components, jet engines, burners, and turbine blades, as they can withstand high temperatures and offer corrosion resistance. The document discusses properties, advantages, disadvantages and applications of CMCs.
This document provides an overview of fatigue failure. It begins by defining fatigue as the premature failure or lowering of strength of a material due to repetitive stresses, even if they are below the material's yield strength. It then discusses key topics in fatigue such as stress cycles, S-N curves, fatigue testing, and factors that affect fatigue life. Crack initiation and propagation stages are described. Methods for improving fatigue performance, such as shot peening and removing stress concentrators, are also covered.
This document provides information about the AE-681 Composite Materials course taught by Dr. PM Mohite. The course covers topics such as introduction to unidirectional composites, analysis of lamina using classical laminate theory, design considerations, micromechanics, and performance under adverse environments. Reference materials include textbooks on composite materials and research papers. Students will be evaluated based on midterm exams, assignments, and a final exam. Attendance will be monitored and late or copied assignments will be penalized.
This document discusses mechanical properties that can be determined from tensile and shear tests. It defines key terms like stress, strain, elastic modulus, yield strength, and tensile strength. A typical stress-strain curve is shown and each region is explained. The elastic portion is linear up to the yield point, then the plastic region involves necking and strain hardening until ultimate failure. True stress and strain account for changes in cross-sectional area during deformation. The document also compares properties like ductility and toughness between different materials.
This document summarizes a student project that studied the mechanical behavior of an aluminum alloy reinforced with alumina and rice husk ash particles. Key points:
- Aluminum alloy 6061 was reinforced with 2% and 4% weight additions of alumina and rice husk ash particles via stir casting.
- Testing showed that the reinforced composites had higher ultimate tensile strength, hardness, flexural strength, and density compared to the unreinforced alloy.
- Microstructural analysis using SEM confirmed good dispersion and retention of the alumina and rice husk ash reinforcement particles in the aluminum matrix.
The document summarizes composites and their classification. It discusses that composites are made of two or more materials to produce new properties. Composites are classified based on the matrix and reinforcement geometry. The main matrix types are polymer, metal, ceramic. Reinforcements include fibers, sheets and particles. Fiber reinforced composites are widely used. Applications of composites include aerospace, automotive, construction, medical and more due to their high strength and stiffness but low density.
Griffith proposed that brittle materials contain fine cracks that concentrate stress below the theoretical strength, causing fracture. When a crack propagates, the new surface area requires energy from the released elastic strain energy of the material. Griffith established that a crack will propagate when the decrease in elastic strain energy is equal to or greater than the energy required to create the new surface. The stress intensity factor describes the stress near a crack tip and is used to predict crack propagation. Fracture toughness is the material property describing a material's resistance to crack propagation.
This document summarizes a seminar presentation on ceramic matrix composites (CMCs). CMCs consist of a ceramic matrix with reinforcements. They offer advantages over monolithic ceramics like higher toughness, strength, and fatigue resistance. Some key applications of CMCs mentioned are in cutting tools, aerospace components, jet engines, burners, and turbine blades, as they can withstand high temperatures and offer corrosion resistance. The document discusses properties, advantages, disadvantages and applications of CMCs.
This document provides an overview of fatigue failure. It begins by defining fatigue as the premature failure or lowering of strength of a material due to repetitive stresses, even if they are below the material's yield strength. It then discusses key topics in fatigue such as stress cycles, S-N curves, fatigue testing, and factors that affect fatigue life. Crack initiation and propagation stages are described. Methods for improving fatigue performance, such as shot peening and removing stress concentrators, are also covered.
The document discusses different types of composite materials including their definitions, advantages, classifications, and properties. It describes metal matrix composites, ceramic matrix composites, and polymer matrix composites. Key points include that composites can have high strength and stiffness yet be lightweight, and that their properties depend on the constituent materials, geometry, and interactions between phases.
This presentation is for mechanical engineering/ civil engineering students to help them understand the different type of destructive mechanical testing of materials. The tensile testing, hardness, impact test procedures are explained in detail.
The document provides information on composites manufacturing technology. It begins with an introduction to composites, their components, characteristics, and classifications. It then discusses various manufacturing processes for composites like hand layup, vacuum bagging, compression molding, and filament winding. The document also includes a case study on the Boeing 787 Dreamliner, highlighting how composites improved its performance and the challenges faced during production. It concludes with advantages and applications of composites in industries like aerospace as well as future developments in nanocomposites and biomedical applications.
This document discusses fracture in materials under tensile loads. It describes two main types of fracture: ductile and brittle. Ductile fracture occurs through plastic deformation and the growth of microvoids, leading to necking of the material before failure. Brittle fracture occurs suddenly without plastic deformation through rapid crack propagation perpendicular to the tensile stress. The document outlines the stages and characteristics of ductile fracture in metals and compares it to the flat, cleavage surfaces of brittle fracture.
Composites consist of a combination of two or more materials, with a matrix and fiber reinforcement. The matrix holds the fibers together and typically transfers stress between fibers. Common matrix materials include polymers and metals. Fibers provide strength and stiffness and can be made of materials like glass, carbon, and Kevlar. Composites offer advantages over traditional materials like high strength to weight ratio, corrosion resistance, and anisotropic properties that allow for tailored designs. However, they also have disadvantages like higher costs and more complex manufacturing compared to metals.
Dynamic Mechanical Analysis (DMA) is a technique that is widely used to characterize a material’s properties as a function of temperature, time, frequency, stress, atmosphere or a combination of these parameters.
The document discusses various types of ceramics and their manufacturing processes. It describes that slurry infiltration and lay-up are two common methods for manufacturing ceramic matrix composites. Slurry infiltration uses capillary forces to infiltrate a slurry into a porous preform, while lay-up involves winding fibers onto a mandrel and hot pressing to consolidate the material. Ceramic matrix composites produced through these methods can have low porosity and good mechanical properties.
Dynamic mechanical properties refer to the response of a material as it is subjected to a periodic force. These properties may be expressed in terms of a dynamic modulus, a dynamic loss modulus, and a mechanical damping term.
This document discusses terminology related to fibre reinforced composites. It defines different types of composites including fibre reinforced polymer composites, laminar composites, and particulate composites. It also defines metal matrix composites. Various fibre materials that are used as reinforcements are discussed such as glass, carbon, and Kevlar fibres. The roles of fibres and factors considered in fibre selection are also summarized.
Ceramic matrix composites (CMCs) consist of ceramic fibers embedded in a ceramic matrix to form a ceramic fiber reinforced ceramic material. They improve the strength and toughness of brittle ceramics. CMCs can be reinforced with either short or continuous fibers. Continuous fiber CMCs provide the best strengthening effect and produce stronger bonding between the fiber and matrix, improving toughness. They exhibit high mechanical strength even at high temperatures, high thermal shock resistance, stiffness, toughness, and thermal and corrosion resistance. CMCs are commonly fabricated using infiltration methods to introduce a ceramic matrix into a fiber preform.
Fatigue is the progressive and localized structural damage that occurs when a material is subjected to fluctuating stresses that are less than the static yield strength of the material. It accounts for about 90% of industrial failures. Fatigue occurs in five stages: cyclic plastic deformation, crack initiation, crack propagation, propagation of macro cracks, and final fracture. It is characterized by beach marks and a rough, brittle fracture surface. Fatigue life can be represented using an S-N curve which plots the maximum stress versus the number of cycles to failure. The fatigue limit or endurance limit is identified as the stress below which a material can undergo any number of stress cycles without failure.
Composites are made by combination of two or more natural or artificial materials to maximize their useful properties and minimize their weaknesses.
Example: The oldest and best-known composites,
Natural: Wood combination of cellulose fibre provides strength and lignin is the "glue" that bonds and stabilizes. Bamboo is a very efficient wood composite structure.
o is a very efficient wood composite structure
Artificial: The glass-fibre reinforced plastic (GRP), combines glass fiber (which are strong but brittle) with plastic (which is flexible) to make a composite material that is tough but not brittle.
70 to 90% of load carried by fibers
Provide structural properties to the composite
Stiffness
Strength
Thermal stability
Provide electrical conductivity or insulation
Example: Glass, Carbon, Organic Boron, Ceramic, Metallic
Function of Fiber/Dispersion phase
This document discusses various types of wear mechanisms that can occur in machines. It defines 11 main types of wear: adhesive, abrasive, erosion, polishing, contact fatigue, corrosive, electro-corrosive, fretting, electrical discharge, cavitation, and false brinelling wear. For each type of wear, it describes the wear process and provides recommendations for both mechanical and lubricant-based prevention methods. Microscopic analysis of wear debris is also discussed as a way to determine the specific type of wear that occurred.
This document discusses composite materials, including their history, components, types, applications, advantages, and disadvantages. Composite materials are composed of two or more constituent materials that differ in composition and remain separate when combined. Historically, Egyptians used mud and straw composites in 1500 BC, while Mongols invented composite bows in the 1200s using wood, bone, and glue. Modern composites use plastics and fibers and have stronger, stiffer, and lighter properties than metals. They contain a matrix, such as polymer, metal, or ceramic, that is reinforced with fibers or particles. Common composites include fiberglass, carbon fiber, and Kevlar in various matrices. Their advantages include tailorable properties while disadvantages include cost
This document discusses super plasticity, which is a deformation process that produces high elongations in metallic materials during tension testing. For super plasticity to occur, the material must have an ultra fine grain size and be deformed at a temperature greater than or equal to 0.4 times the absolute melting point. The document outlines various constitutive relationships that describe super plastic deformation and discusses factors that influence strain rate sensitivity. It also examines conditions necessary for super plastic forming and methods for producing ultrafine grain sizes in materials.
Advanced Composite Materials & Technologies for DefenceDigitech Rathod
This document discusses advanced composite materials and technologies for defense applications. It covers composites for armor applications, including novel ceramic materials and modeling of material response to high-rate loading. It discusses fibers and resins used in ballistic armor composites. Different threats are outlined and the technical requirements for armor are discussed. Body armor design considerations around weight, flexibility and cost are presented.
This document discusses toughness and fracture toughness testing. It defines toughness as the energy absorbed by a material until fracture. Common toughness tests include the Charpy and Izod impact tests, which measure the energy absorbed during a high-velocity impact. However, these tests do not provide data needed for designing with cracks and flaws. Fracture toughness is a better property for design, as it indicates the stress required to propagate a preexisting flaw. The document outlines fracture toughness testing methods like compact tension and single edge notch bending specimens. It also discusses factors that influence fracture toughness values like material thickness, grain orientation, and plane strain versus plane stress conditions.
This document discusses metal matrix composites (MMCs). MMCs consist of a metal matrix reinforced with materials like ceramics or other metals to improve upon the properties of the base metal. Some benefits of MMCs include high strength and stiffness with low weight, improved fatigue and toughness properties compared to metals, and no corrosion issues. MMCs can be made with a variety of matrix and reinforcement combinations and fabricated using common metalworking techniques.
This document discusses out of autoclave composite manufacturing and resin transfer molding (RTM) as alternative processes to traditional autoclave curing. RTM involves placing fiber reinforcement in a closed mold and injecting resin under pressure and heat without an autoclave. The resin cures as it flows through the mold. RTM produces high strength, lightweight composite parts with complex shapes. It is commonly used for aircraft, boat, and wind turbine components. The document provides overviews of RTM and out of autoclave processes, companies that use RTM, benefits, applications, and references for further information.
EFFECT OF NANO RUBBER ADDITIONS ON WEAR AND MECHANICAL PROPERTIES OF EPOXY GL...paperpublications3
Abstract: The use of polymer fiber reinforced composite materials is growing day by day in all types of engineering structures such as aerospace, automotive, aircraft, chemical, constructions etc. because of their tailorable properties. Through these materials are tailorable, improvement in tribological properties is demanded.Keywords:epoxy glass fiber composites, nano nitrile butadiene rubber particles.
EFFECT OF NANO RUBBER ADDITIONS ON WEAR AND MECHANICAL PROPERTIES OF EPOXY GL...paperpublications3
Abstract: The use of polymer fiber reinforced composite materials is growing day by day in all types of engineering structures such as aerospace, automotive, aircraft, chemical, constructions etc. because of their tailorable properties. Through these materials are tailorable, improvement in tribological properties is demanded.Keywords:epoxy glass fiber composites, nano nitrile butadiene rubber particles.
The document discusses different types of composite materials including their definitions, advantages, classifications, and properties. It describes metal matrix composites, ceramic matrix composites, and polymer matrix composites. Key points include that composites can have high strength and stiffness yet be lightweight, and that their properties depend on the constituent materials, geometry, and interactions between phases.
This presentation is for mechanical engineering/ civil engineering students to help them understand the different type of destructive mechanical testing of materials. The tensile testing, hardness, impact test procedures are explained in detail.
The document provides information on composites manufacturing technology. It begins with an introduction to composites, their components, characteristics, and classifications. It then discusses various manufacturing processes for composites like hand layup, vacuum bagging, compression molding, and filament winding. The document also includes a case study on the Boeing 787 Dreamliner, highlighting how composites improved its performance and the challenges faced during production. It concludes with advantages and applications of composites in industries like aerospace as well as future developments in nanocomposites and biomedical applications.
This document discusses fracture in materials under tensile loads. It describes two main types of fracture: ductile and brittle. Ductile fracture occurs through plastic deformation and the growth of microvoids, leading to necking of the material before failure. Brittle fracture occurs suddenly without plastic deformation through rapid crack propagation perpendicular to the tensile stress. The document outlines the stages and characteristics of ductile fracture in metals and compares it to the flat, cleavage surfaces of brittle fracture.
Composites consist of a combination of two or more materials, with a matrix and fiber reinforcement. The matrix holds the fibers together and typically transfers stress between fibers. Common matrix materials include polymers and metals. Fibers provide strength and stiffness and can be made of materials like glass, carbon, and Kevlar. Composites offer advantages over traditional materials like high strength to weight ratio, corrosion resistance, and anisotropic properties that allow for tailored designs. However, they also have disadvantages like higher costs and more complex manufacturing compared to metals.
Dynamic Mechanical Analysis (DMA) is a technique that is widely used to characterize a material’s properties as a function of temperature, time, frequency, stress, atmosphere or a combination of these parameters.
The document discusses various types of ceramics and their manufacturing processes. It describes that slurry infiltration and lay-up are two common methods for manufacturing ceramic matrix composites. Slurry infiltration uses capillary forces to infiltrate a slurry into a porous preform, while lay-up involves winding fibers onto a mandrel and hot pressing to consolidate the material. Ceramic matrix composites produced through these methods can have low porosity and good mechanical properties.
Dynamic mechanical properties refer to the response of a material as it is subjected to a periodic force. These properties may be expressed in terms of a dynamic modulus, a dynamic loss modulus, and a mechanical damping term.
This document discusses terminology related to fibre reinforced composites. It defines different types of composites including fibre reinforced polymer composites, laminar composites, and particulate composites. It also defines metal matrix composites. Various fibre materials that are used as reinforcements are discussed such as glass, carbon, and Kevlar fibres. The roles of fibres and factors considered in fibre selection are also summarized.
Ceramic matrix composites (CMCs) consist of ceramic fibers embedded in a ceramic matrix to form a ceramic fiber reinforced ceramic material. They improve the strength and toughness of brittle ceramics. CMCs can be reinforced with either short or continuous fibers. Continuous fiber CMCs provide the best strengthening effect and produce stronger bonding between the fiber and matrix, improving toughness. They exhibit high mechanical strength even at high temperatures, high thermal shock resistance, stiffness, toughness, and thermal and corrosion resistance. CMCs are commonly fabricated using infiltration methods to introduce a ceramic matrix into a fiber preform.
Fatigue is the progressive and localized structural damage that occurs when a material is subjected to fluctuating stresses that are less than the static yield strength of the material. It accounts for about 90% of industrial failures. Fatigue occurs in five stages: cyclic plastic deformation, crack initiation, crack propagation, propagation of macro cracks, and final fracture. It is characterized by beach marks and a rough, brittle fracture surface. Fatigue life can be represented using an S-N curve which plots the maximum stress versus the number of cycles to failure. The fatigue limit or endurance limit is identified as the stress below which a material can undergo any number of stress cycles without failure.
Composites are made by combination of two or more natural or artificial materials to maximize their useful properties and minimize their weaknesses.
Example: The oldest and best-known composites,
Natural: Wood combination of cellulose fibre provides strength and lignin is the "glue" that bonds and stabilizes. Bamboo is a very efficient wood composite structure.
o is a very efficient wood composite structure
Artificial: The glass-fibre reinforced plastic (GRP), combines glass fiber (which are strong but brittle) with plastic (which is flexible) to make a composite material that is tough but not brittle.
70 to 90% of load carried by fibers
Provide structural properties to the composite
Stiffness
Strength
Thermal stability
Provide electrical conductivity or insulation
Example: Glass, Carbon, Organic Boron, Ceramic, Metallic
Function of Fiber/Dispersion phase
This document discusses various types of wear mechanisms that can occur in machines. It defines 11 main types of wear: adhesive, abrasive, erosion, polishing, contact fatigue, corrosive, electro-corrosive, fretting, electrical discharge, cavitation, and false brinelling wear. For each type of wear, it describes the wear process and provides recommendations for both mechanical and lubricant-based prevention methods. Microscopic analysis of wear debris is also discussed as a way to determine the specific type of wear that occurred.
This document discusses composite materials, including their history, components, types, applications, advantages, and disadvantages. Composite materials are composed of two or more constituent materials that differ in composition and remain separate when combined. Historically, Egyptians used mud and straw composites in 1500 BC, while Mongols invented composite bows in the 1200s using wood, bone, and glue. Modern composites use plastics and fibers and have stronger, stiffer, and lighter properties than metals. They contain a matrix, such as polymer, metal, or ceramic, that is reinforced with fibers or particles. Common composites include fiberglass, carbon fiber, and Kevlar in various matrices. Their advantages include tailorable properties while disadvantages include cost
This document discusses super plasticity, which is a deformation process that produces high elongations in metallic materials during tension testing. For super plasticity to occur, the material must have an ultra fine grain size and be deformed at a temperature greater than or equal to 0.4 times the absolute melting point. The document outlines various constitutive relationships that describe super plastic deformation and discusses factors that influence strain rate sensitivity. It also examines conditions necessary for super plastic forming and methods for producing ultrafine grain sizes in materials.
Advanced Composite Materials & Technologies for DefenceDigitech Rathod
This document discusses advanced composite materials and technologies for defense applications. It covers composites for armor applications, including novel ceramic materials and modeling of material response to high-rate loading. It discusses fibers and resins used in ballistic armor composites. Different threats are outlined and the technical requirements for armor are discussed. Body armor design considerations around weight, flexibility and cost are presented.
This document discusses toughness and fracture toughness testing. It defines toughness as the energy absorbed by a material until fracture. Common toughness tests include the Charpy and Izod impact tests, which measure the energy absorbed during a high-velocity impact. However, these tests do not provide data needed for designing with cracks and flaws. Fracture toughness is a better property for design, as it indicates the stress required to propagate a preexisting flaw. The document outlines fracture toughness testing methods like compact tension and single edge notch bending specimens. It also discusses factors that influence fracture toughness values like material thickness, grain orientation, and plane strain versus plane stress conditions.
This document discusses metal matrix composites (MMCs). MMCs consist of a metal matrix reinforced with materials like ceramics or other metals to improve upon the properties of the base metal. Some benefits of MMCs include high strength and stiffness with low weight, improved fatigue and toughness properties compared to metals, and no corrosion issues. MMCs can be made with a variety of matrix and reinforcement combinations and fabricated using common metalworking techniques.
This document discusses out of autoclave composite manufacturing and resin transfer molding (RTM) as alternative processes to traditional autoclave curing. RTM involves placing fiber reinforcement in a closed mold and injecting resin under pressure and heat without an autoclave. The resin cures as it flows through the mold. RTM produces high strength, lightweight composite parts with complex shapes. It is commonly used for aircraft, boat, and wind turbine components. The document provides overviews of RTM and out of autoclave processes, companies that use RTM, benefits, applications, and references for further information.
EFFECT OF NANO RUBBER ADDITIONS ON WEAR AND MECHANICAL PROPERTIES OF EPOXY GL...paperpublications3
Abstract: The use of polymer fiber reinforced composite materials is growing day by day in all types of engineering structures such as aerospace, automotive, aircraft, chemical, constructions etc. because of their tailorable properties. Through these materials are tailorable, improvement in tribological properties is demanded.Keywords:epoxy glass fiber composites, nano nitrile butadiene rubber particles.
EFFECT OF NANO RUBBER ADDITIONS ON WEAR AND MECHANICAL PROPERTIES OF EPOXY GL...paperpublications3
Abstract: The use of polymer fiber reinforced composite materials is growing day by day in all types of engineering structures such as aerospace, automotive, aircraft, chemical, constructions etc. because of their tailorable properties. Through these materials are tailorable, improvement in tribological properties is demanded.Keywords:epoxy glass fiber composites, nano nitrile butadiene rubber particles.
Wear test of brake friction material on pin on-discSiya Agarwal
The document discusses composite materials and their types, including metal matrix composites, polymer matrix composites, and ceramic matrix composites. It describes the manufacturing processes of liquid state and solid state for metal matrix composites. Applications mentioned include use in carbide drills, defense weapons, and jet landing gear. The document also discusses wear testing done on composite specimens to determine wear rate and coefficient of friction under varying loads. Fiber flax was used instead of asbestos for reinforcement. The composite showed good wear resistance but low tensile strength due to low fiber amount.
Viscoelastic response of polymeric solids in sliding contactspadmanabhankrishnan4
Abstract: The viscoelastic response of polymeric solids to sliding contact conditions
is observed and analyzed with respect to the sliding speed, material composition,
and geometry. It was discovered that polymeric solids produced their own distinct
viscoelastic signatures that cause resonance at certain sliding speeds which can be
explained with resonance conditions for electromagnetic waves. The observed viscolelastic phenomenon is characterized with respect to the relaxation and recovery
times for rigid polymeric solids. It is confirmatory as a demonstration of proof of
existence of viscoelasticity and self-organization in these materials under sliding contact conditions. Viscoelastic observations are also made on the aged specimens in
sliding contact.
This document discusses elastomer applications in new industries and engineering support. It begins with an introduction to elastomers and their properties. It then lists several new industries where elastomers are used, including automotive, aerospace, defense, biomechanics, and consumer products. The document discusses the mechanical behavior of elastomers under different loads. It also discusses elastomer failure modes and how computer simulations can be used to model elastomer behavior and support design. The appendices provide more details on elastomer molecular structure, numerical treatment of incompressibility, and material models based on stretch ratio.
Tensile and Impact Properties of Natural Fiber Hybrid Composite MaterialsIJMER
This paper is a review on the tensile and impact properties of natural fiber hybrid composites.
Natural fibers are having good mechanical properties, high specific strength, low cost, bio-degradable
and easily can recyclable through thermal methods. In this paper two different hybrid composites were
manufactured by compression molding and properties of tensile and impact results are conducted as per
ASTM standards. In this project three different fibers such as sisal, jute and glass with thermosets epoxy
resin used with weight ratio of fiber to resin as 15:15:70.Results showed that sisal/glass hybrid composite
has more tensile and impact strength while comparing to sisal/jute hybrid composite.
This presentation classifies and describes different types of materials:
1) Metals and alloys which have high strength and conductivity but are brittle. Examples include steel, aluminum, and copper.
2) Ceramics like concrete and pottery which are strong under compression but brittle. Examples include refractories and sensors.
3) Polymers or plastics which have lower strength but are lightweight and resistant to chemicals. Examples include polyethylene and epoxy.
4) Semiconductors like silicon that have electrical properties between conductors and insulators, enabling transistors and circuits.
5) Composite materials that combine materials for new properties, like carbon fiber reinforced plastics in aircraft.
INFLUENCE OF RECYCLED RUBBER FILLER ON MECHANICAL BEHAVIOUR OF WOVEN GLASS FI...IAEME Publication
The present work is to determine the mechanical properties of a polymer composite which consist of a vinyl ester as matrix and woven glass fiber (E-glass) filled with milled recycled rubber as reinforcement. The influences of different volume (0%, 3%, 6% and 9%) of the filler on the mechanical properties of the composites were studied. The composite materials are analyzed with the consideration of recycled rubber and without recycled rubber. The mechanical characteristics of these composite materials are compared in terms of young’s modulus and ultimate tensile stress using tensile test and flexural test as per the ASTM standards.
This document summarizes research conducted on modeling and testing a hybrid composite laminate made of glass wool and epoxy resin. Four different types of laminates were prepared by varying the fiber orientation between layers. The laminates were tested for mechanical properties according to ASTM standards. Results showed that increasing cure time improved bonding strength. Changing fiber orientation between layers decreased strength due to delamination. The hybrid laminates were found to have higher strength to weight ratios than steel, indicating their usefulness in applications requiring both strength and light weight. Finite element analysis using ANSYS was also conducted to model stresses in the laminate.
Modeling & Testing Of Hybrid Composite LaminateIOSR Journals
This document summarizes research conducted on modeling and testing a hybrid composite laminate made of glass wool and epoxy resin. Four different types of laminates were prepared by varying the fiber orientation between layers. The laminates were tested for mechanical properties according to ASTM standards. Results showed that increasing cure time improved bonding strength. Changing fiber orientation between layers decreased strength due to delamination. The hybrid laminates were found to have higher strength to weight ratios than steel, indicating their usefulness in applications requiring both strength and light weight. Finite element analysis using ANSYS was also conducted to model stresses in the laminate.
This document provides an introduction to composite materials. It defines composites as materials made of two or more inherently different materials that when combined produce properties exceeding the individual components. The matrix holds the reinforcement and transfers load, while the reinforcement provides properties like strength and stiffness. Common matrix materials include epoxies, metals, and ceramics. Fiber reinforcements include glass, carbon, and aramid fibers. The document discusses different types of composites and their applications, advantages like high strength and design flexibility, and disadvantages like anisotropic properties and difficulties in inspection.
Composites are engineered materials made from two or more constituents with different physical or chemical
properties, which remain separate and distinct within the finished structure. A fiber is a material, which is made into
a long filament with diameter generally in the order of 10 microns. The aspect ratio of length to diameter can be
ranging from thousands to infinity in continuous fibers. Increasing worldwide environmental awareness is
encouraging scientific research into the development of cheaper, more environmentally friendly and more
sustainable construction and packing materials. For environment concern on synthetic fiber (such as glass, carbon,
ceramic gibers etc) natural fibers (such as flax, hemp, jute, kenai) etc are widely used. Industrial hemp fiber is one
of the strongest of the natural fibers available and possesses benefits such as low cost and low production energy
requirements. The primary objective of this research is to fabricate the natural fiber composites with suitable
processing/manufacturing methods and to examine the mechanical properties when subjected to Tension, Bending
and to compare & contrast the results with the available literature. In this research work, hemp fiber reinforced
Epoxy matrix composites have been developed by hand layup method with varying process parameters, such as
coupling agent(with and without compatibilizers) and different fiber percentages (10%,20% and 30% by weight).
The developed composites were then characterized by tensile test and flexural testing. Results show that the tensile
strength and flexural properties increases with the increase in fiber percentage. However after a certain percentage
the tensile strength decreases again. Compared to untreated hemp fiber, no significant changes in the tensile strength
have been observed for treated hemp fiber reinforcement. The flexural strength / modulus of the composite were
higher compared to pure epoxy for all filler/fiber loadings.
Study on Effect of Thickness and Fibre Orientation on a Tensile and Flexural ...IJERA Editor
This project presents the study of tensile, flexural & moisture absorption properties of composites made from S-glass, Carbon and E-glass fibre. The specimens are prepared using hand lay-up techniques as per ASTM standard for different thickness 2mm and 3mm and fibre orientation of 30º, 45º and 60º, where an attempt is made to study the properties of composite materials by composing the different materials together to obtain the desired properties by increasing the thickness and fibre orientation. By the variation of thickness tensile strength of hybrid composite is observed for each thickness and is compared with the finite element analysis results. The test ready specimens were subjected to tensile and flexural loads on UTM. This research indicates that tensile strength is mainly dependent on the fiber orientation & thickness of laminated polymer composites. The moisture absorption increases with the fibre, filler content and duration of immersion in water.
This document presents a study on the effect of thickness and fiber orientation on the tensile and flexural properties of a hybrid composite made from S-glass, carbon, and E-glass fibers. Specimens of different thicknesses (2mm and 3mm) and fiber orientations (30°, 45°, 60°) were prepared and tested according to ASTM standards. The test results showed that tensile strength was dependent on fiber orientation and thickness. Specifically, tensile strength increased with thickness and was highest at a 30° fiber orientation for both the 2mm and 3mm specimens.
Study and Analysis on Mechanical and Wear Behavior of SiC Filled Epoxy Compositepaperpublications3
Abstract: Silicon carbide possesses ample reinforcing potential to be used as a filler material in polymer matrix composites. Successful fabrication of epoxy matrix composites reinforced with silicon carbide particles is possible by simple hand-lay-up technique. These composites possess very low amount of porosity and improved micro-hardness, also it provide slightly superior tensile, flexural and inter-laminar shear strengths than those of the neat epoxy. This study reveals that silicon carbide possesses good filler characteristics as it improves the sliding wear resistance of the polymeric resin. Dry sliding wear characteristics of these composites have been gainfully analysed using a design-of-experiment approach based on Taguchi method. The analysis of experimental results shows that factors like filler content, sliding velocity and normal load, in this sequence, are identified as the significant factors affecting the specific wear rate of the composites under investigation. The silicon carbide-epoxy composites fabricated and experimented upon in this investigation are found to have adequate potential for a wide variety of applications particularly in wear prone environment. When wear is not the predominant degrading factor, epoxy without silicon carbide can be recommended. However, the weight fraction of filler in the composite is to be decided from the view point of required strength. If the place of use is hostile with sliding wear situations, then silicon carbide epoxy composites are to be preferred due to their fairly good wear resistance. Use of these composites may be suggested in applications like engineering structures in dusty environment and low cost building materials in desert.
EXPERIMENTAL STUDY ON WEAR BEHAVIOUR OF SIC FILLED HYBRID COMPOSITES USING TA...IAEME Publication
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1. Dynamic
Properties of
Polymer
Materials
SHORT BOOK - PART III
KARTIK SRINIVAS
BASICS WITH APPLICATIONS
ADVANCED SCIENTIFIC AND ENGINEERING SERVICES (ADVANSES)
REGD. OFFICE: 212, SHUKAN MALL, SABARMATI-GANDHINAGAR HIGHWAY, MOTERA, SABARMATI, AHMEDABAD 380005 INDIA.
PHONE: +91-9624447567 E-MAIL: INFO@ADVANSES.COM HTTP://WWW.ADVANSES.COM
2. Dynamic Testing of Polymer Materials
by
Kartik Srinivas
Managing Principal
CAE & Material Testing Services, AdvanSES
Phone: +91-9624447567; E-mail: info@advanses.com
Advanced Scientific and Engineering Services (AdvanSES)
212, Shukan Mall, Sabarmati-Gandhinagar Highway
Motera, Sabarmati, Ahmedabad 380005 India.
http://www.advanses.com
3. To,
Dr. Ken Cornelius (Professor, Wright State University, Dayton, OH)
Bob Samples (Founder, Akron Rubber Development Lab., Akron, OH)
My Parents, Santha and M. S. Srinivasan,
Subha and Advait
5. Chapter 1
Dynamic Testing of Polymer Materials
1.1 Introduction
Naturally occuring polymers like wood, rubber, silk, etc. have been used for a long time
owing to benefits such as ease of availablility, environmental compatibility, and suitability
for various applications. Natural rubber, a naturally occuring elastomer is made from latex
extracted from the plant Hevea brasiliensis. Malaysia, India, Thailand and Indonesia are
some of the largest rubber manufacturing countries. The latex plant grows in tropical cli-
mates and once the trees are 4 to 6 years old they can be harvested. Latex is tapped from
the sap of the tree by making incisions deep enough to tap the latex carrying vessels. The
tapped latex is collected and stored at a suitable location for further processing. Natural
rubber in its raw state is made up of long chains of polymers, which in turn are made of
small molecules called monomers. It is sticky, and deforms easily at room temperature
and not particularly useful as an engineering material. The properties of rubber are made
engineering friendly by the process of vulcanization. The credit for the discovery of vul-
canization goes to Charles Goodyear. Vulcanization is the process of sulphurizing the gum
rubber, where crosslinks are formed between the polymer chains and sulphur. Crosslinking
makes the rubber elastic and is responsible for providing the rubber with hardness, stiffness
and other engineering properties.
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6. Synthetic rubber is made in a laboratory from petroleum by products. Fritz Hofmann
is credited with the discovery of synthetic rubber in 1909. The development of synthetic
rubber took place in the first decades of the twentieth century. The development of syn-
thetic rubber gave rise to elastomer compounding as a science. Synthetic elastomers were
developed to obtain characterisitics like high temperature resistance, marine compatibility,
resistance to industrial oils etc. Synthesization of different types of new rubber materials in
the past few decades has led to some novel elastomers and composites that have replaced
the use of traditional metals in many applications. China is the largest manufacturer and
consumer of synthetic rubber.
Steel, aluminum and other materials are combined with soft elastomers to design prod-
ucts that can provide specific deformation characterisitics. The elastomer provides the
flexibility or compliance and steel provides the required directional stiffness. Applications
as automotive bushings, bridge bearing pads, spherical laminated bearings etc., utilize the
bimaterial design to provide the required deformation characteristics and shear strain ca-
pabilities. Tire design utilizes rubber so as to provide variable stiffness characteristics at
different locations of the tire. The tread rubber provides frictional resistance combined
with high strain capabilities. The side-wall rubber provides fatigue resistance combined
with lower stiffness and the wedge rubber is made up of soft material to provide fatigue
resistance from repeated shear straining. A generic sports utility vehicle tire is sometimes
made up of upto twenty different kinds of rubbers to provide the required ride and defor-
mation characteristics. A passenger car typically has about 650 rubber components.
Figure(1.1) shows the typical stress-strain curves for three main types of polymeric ma-
terials. The first curve shows the behavior of a brittle polymer, where the failure is sudden
as soon as the ultimate stress is reached. This class of materials show high hardness and
behavior similar to ceramic materials. The second curve shows the behavior of a polymer
similar to many metals, as can be observed there is a definite yield point and a harden-
ing region before the ultimate failure. This polymer exhibits a plastic behavior beyond
their elastic limits. The third curve shows the behavior of a typical elastomer. This curve
shows that the material can handle large recoverable strains without undergoing permanent
deformations. The characterisitic of the material to undergo repeated deformations with-
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7. out showing a set is termed as Hyperelasticity. The nonlinear nature of the curve shows the
continuous change in modulus of elasticity with respect to the strain levels. The ”Modulus”
in elastomer parlance is the value of stress at a particular value of strain.
Figure 1.1: Stress-Strain Curves for Polymers
1.2 Dynamic Properties
Static testing of materials as per ASTM D412, ASTM D638, ASTM D624 etc can be cate-
gorized as slow speed tests or static tests. The difference between a static test and dynamic
test is not only simply based on the speed of the test but also on other test variables em-
ployed like forcing functions, displacement amplitudes, and strain cycles. The difference
is also in the nature of the information we back out from the tests. When related to poly-
mers and elastomers, the information from a conventional test is usually related to quality
control aspect of the material or the product, while from dynamic tests we back out data
regarding the functional performance of the material and the product.
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8. Figure 1.2: Purely Elastic and Purely Viscous Responses of Materials
Polymer materials are widely used in all kinds of engineering applications because of
their superior performance in vibration isolation, impact resistance, rate dependency and
time dependent properties. In some traditional applications they have consistently shown
better performance combining with other materials like glass fibers etc.,and are now re-
placing metals and ceramics in such applications. The investigations of polymer properties
in vibration, shock, impact and other viscoelastic phenomena is now considered critical,
and understanding of dynamic mechanical behaviour of polymers becomes necessary and
compulsory.
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9. Figure 1.3: Dynamic Stiffness of a Polymer Material
Characterization of dynamic properties play an important part in comparing mechanical
properties of different polymers for quality, performance prediction, failure analysis and
new material qualification. Figures 1.2 and 1.4 show the responses of purely elastic, purely
viscous and of a viscoelastic material. In the case of purely elastic, the stress and the strain
(force and resultant deformation) are in perfect sync with each other, resulting in a phase
angle of 0. For a purely viscous response the input and resultant deformation are out of
phase by 90o. For a viscoleastic material the phase angle lies between 0 and 90o. Generally
the measurements of viscoelastic materials are rerepresented as a complex modulus E* to
capture both viscous and elastic behavior of the material. The stress is the sum of in-phase
response and out-of-phase responses.
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10. Figure 1.4: Viscoelastic Response of a Polymer Material
1.3 Instruments for Dynamic Testing of Polymers
There are five (5) main classes of experiments for measurement of viscoelastic behaviour
1. Transient measurements: creep and stress relaxation
2. Low frequency vibrations: free oscillations methods
3. High frequency vibrations: resonance methods
4. Forced vibration non-resonance methods
5. Wave propagation methods
The frequency scale for the different test methods are shown in Figure(1.5)
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11. Figure 1.5: Frequency Scale for Different Test Methods
Dynamic characterization of elastomeric materials and polymers requires the use of so-
phisticated instruments with high fidelity load cells, displacement transducers and strain
gauges to understand the deformations taking place in the material under dynamic frequen-
cies. A Rheometer is used to test the dynamic properties during cure. A servo hydraulic
fatigue testing machine and dynamic mechanical analyzer (DMA) instruments are the pri-
mary material testing instruments used in dynamic characterization of polymers. The so-
phistication of material testing instruments increase with needs for higher frequencies and
higher loads. Strain gauge based and piezoelectric quartz based load cells are used in this
instruments to study the load, stress and strain and record the test data.
Along with high quality hardware need also arises for a sophisticated and advanced
software to carry out all the calculations. The software that calculates all the dynamic
properties also needs to be as sophisticated and advanced as the hardware required to do
the test
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12. Figure 1.6: AdvanSES High Frequency and ElectroMechanical Testing Setup
Figure(1.6) shows the AdvanSES servo hydraulic tester used in material testing at high
frequencies the servo hydraulic tester is capable of going up to 100 hertz under sine wave
definition hydraulic actuator is the primary source of frequency generation in the instrument
and the servo valve in the actuator controls the flow of hydraulic fluid into the actuator so as
to apply a controlled displacemtn at controlled frequency. The load cell in the instrument
measures the loads generated in the sample under the dynamic frequencies. The servo
hydraulic tester is primary primarily used to study static and dynamic stiffness, loss and
storage modulus and Tan-delta. Fatigue crack growth propagation of rubber samples can
also be tested using a high fps camera integrated with the tester. Elevated temperature
testing is also available with the use of a temperature chamber with automatic PID control.
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13. Figure 1.7: AdvanSES High Frequency Testing Setup with Temperature Chamber
High temperature tests (e.g. tensile, compression, flexure and fatigue tests) are used to
determine the thermal-elastic behavior, heat resistance, endurance and durability of metal-
lic and polymer materials. Elevated temperatures is combined with mechanical testing,
environmental aging, analytical solution methods to develop and provide a comprehensive
test protocol to evaluate materials and components.
Figure 1.8: Oscillating Rheometer for Dynamic Testing
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14. Figure(1.8) shows a rheometer instrument used for studying the dynamic properties of
uncured and cured rubber compounds. The instrument consists of a torque applicator, an
oscillator and a load measuring device. The sample is held between the torque bar and
the cup. The oscillator supplies an oscillatory motion that is transferred to the sample by
the cup. The angular torsional deformations of the sample and the load generated in the
instrument are measured using advanced load cell, displacement transducers and rotary
encoders. A sine wave is input into the sample and a sine wave is similarly output from the
instrument, both the input and output waves are compared to calculate the storage modulus,
loss modulus and the tangent delta.
The sample requirements for the rheometer testing are that the samples should be di-
mensionally stable of rectangular or cylindrical cross section. To test the material a sample
is firmly gripped at both ends. the specimen is electromagnetically or servo driven into
sinusoidal oscillations of defined amplitude and frequency. The viscoelastic properties of
the material makes the torque lag behind the deformation. The lag between the input and
output is the phase angle as shown earlier in Figure(1.4). The observed values for load,
phase angle, and geometry constant of the specimen is used to calculate the complex shear
modulus G*, the storage shear modulus G’, the loss shear modulus G”, and tan delta.
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15. Figure 1.9: Axial Dynamic Mechanical Analyzer with Furnace
Figure(1.9) shows a DMA instrument manufactured buy TA Instruments. As shown in
the figure, a force motor with a coil and magnet is used to apply a force and lvdt measures
the displacement of the sample. Furnace is provided for elevated and low temperature
measurements. The sample is kept inside the furnace and a sine wave is input into the force
motor, the resultant sine wave voltage of the lvdt is now compared to the input sine wave
and the storage modulus, loss modulus, phase and tan delta are calculated from the test
results data.
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16. Figure 1.10: Axial Dynamic Mechanical Analyzer with Interchangable Sample Fixtures.
Image Courtesy: Perkin Elmer Industries
Figure(1.10) shows a DMA instrument from Perkin Elmer. When compared to the TA
Instruments, both the machines have similar performance. Both the instruments can be
operated under stress control and strain control. Creep and stress relaxation experiments
can be carried out in all the instruments along with frequency sweep, strain sweep and
temperature sweep studies
A DMA instrument is very versatile instrument able to apply different deformation
modes on the sample. Different deformation modes can be chosen based upon the quality
of the material and the material properties under study. Figure(1.11) shows the different
deformation modes available for application in a DMA instrument. Single and double
cantilever beam, tensile, shear, compression and three point bending tests can be carried
out using different kinds of fixtures.
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17. Figure 1.11: Deformation Modes Available in a Typical DMA Machine, Image Courtesy:
TA Instruments and Perkin Elmer Industries
Materials such as hard polymers or soft viscoelastic elastomers are ideal materials to be
tested on a DMA machine for dynamic properties. The testing conditions and parameters
such as applied frequency range, temperature and available sample sizes and shape dictate
the machine required for the testing. To carry out frequency and strain sweep studies on
automotive and aerospace components, it becomes imperative to use a servo hydraulic
machine. While the necessity to study the dynamic property of a material during processing
makes it imperative to use a moving or oscillating die rheometer.
The importance of dynamic testing comes from the fact that performance of elastomers
and elastomeric products such as engine mounts, suspension bumpers, tire materials etc.,
cannot be fully predicted by using only traditional methods of static testing. Elastomer
tests like hardness, tensile, compression-set, low temperature brittleness, tear resistance
tests, ozone resistance etc., are all essentially quality control tests and do not help us under-
stand the performance or the durability of the material under field service conditions. An
elastomer is used in all major applications as a dynamic part being able to provide vibra-
Page 13 c Kartik Srinivas
18. tion isolation, sealing, shock resistance, and necessary damping because of its viscoelastic
nature. Dynamic testing truly helps us to understand and predict these properties both at
the material and component level.
1.4 ASTM D5992 and ISO 4664-1
ASTM D5992 covers the methods and process available for determining the dynamic prop-
erties of vulcanized natural rubber and synthetic rubber compounds and components. The
standard covers the sample shape and size requirements, the test methods, and the pro-
cedures to generate the test results data and carry out further subsequent analysis. The
methods described are primarily useful over the range of temperatures from cryogenic to
200◦C and for frequencies from 0.01 to 100 Hz, as not all instruments and methods will
accommodate the entire ranges possible for material behavior.
Figures(1.12 and 1.13) show the results from a frequency sweep test on five (5) different
elastomer compounds. Results of Storage modulus and Tan delta are plotted.
Figure 1.12: Plot of Storage Modulus Vs Frequency from a Frequency Sweep Test
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19. Figure 1.13: Plot of Tan delta Vs Frequency from a Frequency Sweep Test
The frequency sweep tests have been carried out by applying a pre-compression of
10 % and subsequently a displacement amplitude of 1 % has been applied in the positive
and negative directions. Apart from tests on cylindrical and square block samples ASTM
D5992 recommends the dual lap shear test specimen in rectangular, square and cylindrical
shape specimens. Figure(1.14) shows the double lap shear shapes recommended in the
standard.
Page 15 c Kartik Srinivas
21. 1.5 References
1. Sperling, Introduction to Physical Polymer Science, Academic Press, 1994.
2. Ward et al., Introduction to Mechanical Properties of Solid Polymers, Wiley, 1993.
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5. Goldman, Prediction of Deformation Properties of Polymeric and Composite Mate-
rials, ACS, 1994.
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and Structures, 2003.
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tomers, Rubber Chemistry and Technology, Vol. 72, 2000.
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Biological Tissues with Examples, Applied Mechanics Review, Vol. 40, No. 12,
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Materials, Transactions of the Society of Rheology, Vol. 6, 1962.
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22. 15. Eberhard Meinecke, Effect of Carbon-Black Loading and Crosslink Density on the
Heat Build-Up in Elastomers, Rubber Chemistry and Technology, Vol. 64, May
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16. Boyce, M. C., and Arruda, E. M., Constitutive Models of Rubber Elasticity: A Re-
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and Sons, NY, 1999.
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1998.
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tion of Two Engineering Thermoplastic Polymers in Contact with Ethanol Fuel from
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21. Menard, Kevin, P., Dynamic-Mechanical Analysis, CRC Press, Boca Raton, 1999.
22. Nielsen, L. E., Mechanical Properties of Polymers, Marcel Dekker, New York, 1974.
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23. 27. Srinivas, K., Systematic Experimental and Computational Mechanics Failure Analy-
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24. 40. Sasso, M., Palmieri, G., Chiappini, G., and Amodio, D. Characterization of hypere-
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51. Perkin Elmer Industries, Class Notes and Machine Manuals, 2007.
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25. 53. Danko, D. M., and Svarovsky, J. E., An Application of Mini-Computers for the De-
termination of Elastomeric Damping Coefficients and Other Properties, SAE Paper
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Page 21 c Kartik Srinivas
26. Kartik Srinivas
Kartik Srinivas has a Master's degree in Mechanical Engineering from Wright State University, USA.
He is a consulting mechanical polymer engineer with extensive background and experience in
product engineering using simulation technologies and mechanical testing. He started his career as
a consulting Mechanical/FEA Engineer at Akron Rubber Development Laboratory, Akron, Ohio,
USA. In a career of over a decade and half in USA and at Advanced Scientific and Engineering
Services (AdvanSES) India, Kartik has advised and assisted companies solve engineering
problems related to elastomeric, thermoplastic and TPE materials. Kartik provides material and
design development, material testing, Finite Element Analysis (FEA) solutions to a broad range of
industries and is well versed with material and product testing as per ASTM and ISO standards. In
his professional career he has worked with industry leading OEMs, Tier 1 and 2 suppliers providing
product R&D, material development and testing, design optimization, reverse engineering and
manufacturing services. Kartik Srinivas has 7 technical papers to his credit and has been the chair
of the session on automotive composites at the SAE World Congress from 2006 through 2011. He
has volunteered as a reviewer for the Journal of Rubber Chemistry and Technology.
AdvanSES' Laboratory and Workshop near Ahmedabad, India
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