In a tension test on a ductile material, a diffuse necking - so called because its spatial extension is much larger than the sheet thickness - begins to develop in the sample when the strain hardening is no longer able to compensate for the weakening due to the reduction of the cross section. After some elongation under decreasing load, a localized neck usually appears in the region of the diffuse neck. In the localized neck, severe thinning occurs leading to ultimate failure.
This work focuses on studying the diffuse and localized necking under plane stress conditions in visco-plastic materials under dynamic loading. By means of a DOE analysis the main material parameters that influence the occurrence of local and diffuse necking were determined. A material model is then validated by systematic comparison of simulation results with physical tests carried out at different strain rates. One methodology to achieve good correlation between test and experiments is the use of a damage model. The damage model chosen by the authors is GISSMO (Generalized Incremental Stress-State dependent damage Model), due to its widespread usage in the crash community.
The GISSMO model is defined in terms of a critical plastic strain that indicates the start of damage coupling and a failure plastic strain indicating fracture, both are defined as a function of stress triaxiality. As the necking or more generally plastic instability will result in mesh dependency of the simulation results, regularization is introduced by defining both the failure plastic strain and the damage exponent as a function of the mesh size. As the spatial extension of the diffuse neck differs as a function of strain rate, one way to achieve correlation between test and simulation is to express these parameters as function of both the mesh size and the strain rate.
As consequence of the findings of this study, a number of new options were developed in the GISSMO model.
Fatigue is important as it is the largest cause of failure in metals, estimated to comprise approximately 90% of all metallic failures; polymers and ceramics are also susceptible to this type of failure.
Types of stresses and theories of failure (machine design & industrial drafti...Digvijaysinh Gohil
This document summarizes different types of stresses and theories of failure in mechanical components. It discusses eight types of stresses: tensile, compressive, bending, direct shear, torsional shear, bearing pressure, crushing, and contact stresses. It then explains three main theories of failure - maximum principal stress theory, maximum shear stress theory, and distortion energy theory - and their applications based on the material properties.
Recrystallization is the process in which deformed grains of the crystal structure are replaced by a new set of stress-free grains that nucleate and grow until all the original grains have been consumed. The process is accomplished by heating the material to temperatures above that of crystallization.
Its a class lecture about Centrifugal Casting in Production Process subject. This class held at Khulna University of Engineering & Technology. Class conducted by Md. Abdullah Al Bari.
The document discusses the design and analysis of a composite leaf spring. It begins with an abstract that outlines replacing steel leaf springs with composite materials to reduce weight. It then provides sections on leaf springs, composite materials, literature reviews on previous composite leaf spring research, and the project overview which involves designing leaf springs in CATIA and analyzing them in ANSYS. The document provides details on the material properties, design calculations, and modeling and analysis procedures.
Fatigue is important as it is the largest cause of failure in metals, estimated to comprise approximately 90% of all metallic failures; polymers and ceramics are also susceptible to this type of failure.
Types of stresses and theories of failure (machine design & industrial drafti...Digvijaysinh Gohil
This document summarizes different types of stresses and theories of failure in mechanical components. It discusses eight types of stresses: tensile, compressive, bending, direct shear, torsional shear, bearing pressure, crushing, and contact stresses. It then explains three main theories of failure - maximum principal stress theory, maximum shear stress theory, and distortion energy theory - and their applications based on the material properties.
Recrystallization is the process in which deformed grains of the crystal structure are replaced by a new set of stress-free grains that nucleate and grow until all the original grains have been consumed. The process is accomplished by heating the material to temperatures above that of crystallization.
Its a class lecture about Centrifugal Casting in Production Process subject. This class held at Khulna University of Engineering & Technology. Class conducted by Md. Abdullah Al Bari.
The document discusses the design and analysis of a composite leaf spring. It begins with an abstract that outlines replacing steel leaf springs with composite materials to reduce weight. It then provides sections on leaf springs, composite materials, literature reviews on previous composite leaf spring research, and the project overview which involves designing leaf springs in CATIA and analyzing them in ANSYS. The document provides details on the material properties, design calculations, and modeling and analysis procedures.
Fatigue and creep are fundamental mechanical properties of materials. Fatigue is the failure of a material caused by repeated application of cyclic stresses, even if the stresses are below the yield strength of the material. It can lead to loss of strength, ductility, and uncertainty in service life. Creep is the slow deformation of materials under a constant load at high temperatures. Creep deformation occurs in three stages - primary, secondary, and tertiary. Factors like temperature, grain size, heat treatment, and alloying elements affect the fatigue and creep properties of materials. Mechanisms like dislocation climb, vacancy diffusion, and grain boundary sliding contribute to creep deformation at high temperatures.
Tribology is the study of friction, lubrication, and wear between interacting surfaces in relative motion. It helps improve machine reliability and reduce failures. Reynolds' equation, derived in 1886, quantifies fluid film lubrication and allows prediction of hydrodynamic, hydrostatic, and squeeze film mechanisms by modeling pressure as a function of coordinates and time. The equation assumes laminar flow of an incompressible Newtonian fluid with negligible inertia and pressure gradients in the film thickness direction.
efect of ductile to brittle transition temperturesanjay sahoo
This document summarizes a seminar on how the ductile to brittle transition temperature (DBTT) can affect ships. It discusses how the Titanic's steel structure failed due to brittle fracture from low temperatures. The DBTT is the temperature at which a material changes from ductile to brittle behavior. Several factors can influence a material's DBTT curve, including crystal structure, grain size, heat treatment, and composition. Modern steels have lower sulfur contents and smaller grains, leading to higher transition temperatures than the steel used for the Titanic. Understanding how materials behave at low temperatures helps make ships safer by considering fracture risks during design.
Cold isostatic pressing (CIP) is a technique where high pressure is applied uniformly to metal powder sealed in a flexible container. This compacts the powder to a density of 75-85% without die wall friction, resulting in a part with uniform density and no residual stresses. There are two methods - the wet bag process suited for batch production of complex parts, and the dry bag process using a fixed mold for mass production. CIP is used to make intricate or long shapes out of materials like titanium, tool steels, tungsten, and molybdenum powders.
This document presents the design of a screw jack. The screw jack is intended to lift a 3500 kg car to a height of 200 mm during maintenance work. It will utilize a screw and nut mechanism to convert rotational force into linear lifting force. The objectives are to design, select materials for, and dimension the screw jack. The methodology will involve referring to textbooks on machine design, strength of materials, and materials science. The design concepts to be considered include cost, strength, mechanical properties, and physical properties of the materials. Limitations include not accounting for dynamic or impact loading, requiring a safety factor of 5 or more to mitigate risks of failure from these loads. Drawings and specifications for the screw jack components will be developed.
This document discusses stresses in different types of pressure vessels. It describes stresses in thin cylindrical and spherical shells due to internal pressure, including circumferential/hoop stress and longitudinal stress. It also covers thick cylindrical shells and uses Lame's equation to calculate stresses at different radii. It provides equations for determining wall thickness of thin and thick shells made of both brittle and ductile materials. Compound cylindrical shells and stresses within are also addressed.
Thixocasting or semi solid metal castingIlyas Hussain
Thixocasting is a near-net shape forming process that uses partially molten alloys. It involves three steps: 1) Producing a pre-cast billet with a globular microstructure through electromagnetic stirring, 2) Reheating the billet to the semi-solid temperature, and 3) Casting the component by pressing the billet into a die cavity. Thixocasting provides benefits like energy efficiency, dimensional accuracy, and fine microstructures. However, it requires strict control of parameters like temperature and stirring. Common applications include automotive components like engine mounts and housings.
DESIGN AND ANALYSIS OF LEAF SPRING BY USING COMPOSITE MATERIAL FOR LIGHT VEHI...IAEME Publication
The document describes the design and analysis of a composite leaf spring to replace the steel leaf spring on a Mahindra Commander 650 DI light vehicle. Leaf springs are commonly used for vehicle suspension but are heavy. The goal was to design a composite leaf spring using glass fiber reinforced polymer (E-glass/epoxy) that is lighter than the steel spring while maintaining stiffness. The composite leaf spring design was modeled in Pro/ENGINEER and analyzed in ANSYS software. Results showed the composite leaf spring design weighed 85% less than the steel design while meeting the stiffness requirements.
Fiber Re-inforced composites introductionHareesh K
This document provides an introduction to fiber-reinforced composites. It discusses the history of composites beginning in the 1940s when they were used to create lightweight materials for military vehicles. It defines composites as materials made from two or more constituent materials that produce properties different from the individual components. The document outlines the characteristics of fiber-reinforced composites and provides examples of their applications in aircraft, space vehicles, automobiles, sporting goods, marine vessels, and infrastructure. It also discusses the material selection process for composites.
Sliding Contact Bearing Theory Prof. Sagar DhotareSagar Dhotare
In present ppt covers following points:
Introduction of Sliding Contact Bearings
Classification
Applications
Different lubrications systems
Hydrodynamic bearing concept and working
Comparison between sliding and rolling contact bearings
PETROFF’S EQUATION For Hydrodynamic Journal Bearing
Dimensionless Parameters used in SCB
Design procedure for Hydrodynamic Journal Bearing
Fatigue is a type of failure caused by fluctuating stresses that are lower than the material's yield stress. It results from the initiation and propagation of cracks under cyclic stresses. Fatigue failure can occur suddenly in ductile materials without prior plastic deformation. The S-N curve relates the cyclic stress amplitude to the number of cycles until failure. It may show a fatigue limit below which failure will not occur even after an infinite number of cycles for some materials like steels. Non-ferrous materials typically do not have a fatigue limit.
Extruders: defects and troubleshooting.pptxAbhijithKS36
The slide contains details of most common defects and troubleshooting(reason, causes, remedy) of polymer extruders used in industries for various types of polymer product manufacturing.
Mumbai University
Mechanical engineering
SEM III
Material Technology
Module 1.4
Strain Hardening:
Definition importance of strain hardening, Dislocation theory of strain hardening, Effect of strain hardening on engineering behaviour of materials, Recrystallization Annealing: stages of recrystallization annealing and factors affecting it
The document discusses three microstructural transformations: recovery, recrystallization, and grain growth that occur during annealing of cold worked materials. Recovery involves a reduction in point defects and dislocation rearrangement into low energy configurations at low annealing temperatures. Recrystallization occurs at higher annealing temperatures and results in the formation of new strain-free grains. Grain growth follows recrystallization and leads to an increase in the average grain size as larger grains grow at the expense of smaller ones.
1. The document discusses fatigue, which is structural damage that occurs when a material is subjected to cyclic loading below its tensile strength.
2. It describes how fatigue occurs through repeated loading and unloading causing microscopic cracks, and how factors like stress concentration, material properties, and the environment affect fatigue life.
3. The document outlines an experiment to determine the fatigue life of aluminum specimens under different stress levels using a fatigue testing machine. Results are analyzed to find the safe stress level for 1 million reversals.
It is a near net shape process in which casting and forging is done in single step.
It is Referred by many names such as “squeeze casting” , “pressure infiltration”, “liquid metal forging”, “extrusion casting”, “liquid pressing'', “pressure crystallization”.
The document presents a study on fabricating and characterizing an aluminum metal matrix composite reinforced with silicon carbide particles. The objectives are to fabricate the Al-SiC MMC, characterize its tensile strength and hardness properties, and determine optimal machining parameters for good surface finish. It discusses the composite materials, matrix, reinforcement, classification of composites, and metal matrix composites. It also details the properties of aluminum, silicon carbide, and aluminum silicon carbide composites. Methods of fabricating Al-SiC MMC including stir casting and characteristics like tensile testing, hardness testing, and machining tests are explained. Relevant literature on improving mechanical properties of Al-SiC composites is reviewed.
Flexibility Analysis In Industrial Piping Through The Finite Elements And Pho...IJERA Editor
This document analyzes the flexibility of industrial piping through finite element analysis, photoelasticity, and mathematical modeling. It presents the equations and properties used in each modeling method. The finite element model in ANSYS showed stress distributions that matched the mathematical model. The photoelasticity model allowed visualizing stress curves but values were difficult to obtain. The computational finite element model was determined to be best for industrial applications by providing reliable stress and deformation values and allowing complex analyses.
IRJET-Finite Element Analysis of Seat Belt Buckle AssemblyIRJET Journal
This study analyzed a seat belt buckle assembly using finite element analysis to determine the total deformation and von Mises stress under different loading conditions and thickness variations. A 3D model of the seat belt buckle was created in Solid Edge and meshed. The assembly was analyzed for loads of 63.5N to 350N and thicknesses of 8mm to 4mm. Results showed that total deformation and stress increased as thickness decreased, with a maximum deformation of 0.00125mm and maximum stress of 32.87MPa. The buckle's ultimate strength is 300MPa, so stresses remained well below the failure point. Thinner designs reduced material usage while maintaining structural integrity.
Fatigue and creep are fundamental mechanical properties of materials. Fatigue is the failure of a material caused by repeated application of cyclic stresses, even if the stresses are below the yield strength of the material. It can lead to loss of strength, ductility, and uncertainty in service life. Creep is the slow deformation of materials under a constant load at high temperatures. Creep deformation occurs in three stages - primary, secondary, and tertiary. Factors like temperature, grain size, heat treatment, and alloying elements affect the fatigue and creep properties of materials. Mechanisms like dislocation climb, vacancy diffusion, and grain boundary sliding contribute to creep deformation at high temperatures.
Tribology is the study of friction, lubrication, and wear between interacting surfaces in relative motion. It helps improve machine reliability and reduce failures. Reynolds' equation, derived in 1886, quantifies fluid film lubrication and allows prediction of hydrodynamic, hydrostatic, and squeeze film mechanisms by modeling pressure as a function of coordinates and time. The equation assumes laminar flow of an incompressible Newtonian fluid with negligible inertia and pressure gradients in the film thickness direction.
efect of ductile to brittle transition temperturesanjay sahoo
This document summarizes a seminar on how the ductile to brittle transition temperature (DBTT) can affect ships. It discusses how the Titanic's steel structure failed due to brittle fracture from low temperatures. The DBTT is the temperature at which a material changes from ductile to brittle behavior. Several factors can influence a material's DBTT curve, including crystal structure, grain size, heat treatment, and composition. Modern steels have lower sulfur contents and smaller grains, leading to higher transition temperatures than the steel used for the Titanic. Understanding how materials behave at low temperatures helps make ships safer by considering fracture risks during design.
Cold isostatic pressing (CIP) is a technique where high pressure is applied uniformly to metal powder sealed in a flexible container. This compacts the powder to a density of 75-85% without die wall friction, resulting in a part with uniform density and no residual stresses. There are two methods - the wet bag process suited for batch production of complex parts, and the dry bag process using a fixed mold for mass production. CIP is used to make intricate or long shapes out of materials like titanium, tool steels, tungsten, and molybdenum powders.
This document presents the design of a screw jack. The screw jack is intended to lift a 3500 kg car to a height of 200 mm during maintenance work. It will utilize a screw and nut mechanism to convert rotational force into linear lifting force. The objectives are to design, select materials for, and dimension the screw jack. The methodology will involve referring to textbooks on machine design, strength of materials, and materials science. The design concepts to be considered include cost, strength, mechanical properties, and physical properties of the materials. Limitations include not accounting for dynamic or impact loading, requiring a safety factor of 5 or more to mitigate risks of failure from these loads. Drawings and specifications for the screw jack components will be developed.
This document discusses stresses in different types of pressure vessels. It describes stresses in thin cylindrical and spherical shells due to internal pressure, including circumferential/hoop stress and longitudinal stress. It also covers thick cylindrical shells and uses Lame's equation to calculate stresses at different radii. It provides equations for determining wall thickness of thin and thick shells made of both brittle and ductile materials. Compound cylindrical shells and stresses within are also addressed.
Thixocasting or semi solid metal castingIlyas Hussain
Thixocasting is a near-net shape forming process that uses partially molten alloys. It involves three steps: 1) Producing a pre-cast billet with a globular microstructure through electromagnetic stirring, 2) Reheating the billet to the semi-solid temperature, and 3) Casting the component by pressing the billet into a die cavity. Thixocasting provides benefits like energy efficiency, dimensional accuracy, and fine microstructures. However, it requires strict control of parameters like temperature and stirring. Common applications include automotive components like engine mounts and housings.
DESIGN AND ANALYSIS OF LEAF SPRING BY USING COMPOSITE MATERIAL FOR LIGHT VEHI...IAEME Publication
The document describes the design and analysis of a composite leaf spring to replace the steel leaf spring on a Mahindra Commander 650 DI light vehicle. Leaf springs are commonly used for vehicle suspension but are heavy. The goal was to design a composite leaf spring using glass fiber reinforced polymer (E-glass/epoxy) that is lighter than the steel spring while maintaining stiffness. The composite leaf spring design was modeled in Pro/ENGINEER and analyzed in ANSYS software. Results showed the composite leaf spring design weighed 85% less than the steel design while meeting the stiffness requirements.
Fiber Re-inforced composites introductionHareesh K
This document provides an introduction to fiber-reinforced composites. It discusses the history of composites beginning in the 1940s when they were used to create lightweight materials for military vehicles. It defines composites as materials made from two or more constituent materials that produce properties different from the individual components. The document outlines the characteristics of fiber-reinforced composites and provides examples of their applications in aircraft, space vehicles, automobiles, sporting goods, marine vessels, and infrastructure. It also discusses the material selection process for composites.
Sliding Contact Bearing Theory Prof. Sagar DhotareSagar Dhotare
In present ppt covers following points:
Introduction of Sliding Contact Bearings
Classification
Applications
Different lubrications systems
Hydrodynamic bearing concept and working
Comparison between sliding and rolling contact bearings
PETROFF’S EQUATION For Hydrodynamic Journal Bearing
Dimensionless Parameters used in SCB
Design procedure for Hydrodynamic Journal Bearing
Fatigue is a type of failure caused by fluctuating stresses that are lower than the material's yield stress. It results from the initiation and propagation of cracks under cyclic stresses. Fatigue failure can occur suddenly in ductile materials without prior plastic deformation. The S-N curve relates the cyclic stress amplitude to the number of cycles until failure. It may show a fatigue limit below which failure will not occur even after an infinite number of cycles for some materials like steels. Non-ferrous materials typically do not have a fatigue limit.
Extruders: defects and troubleshooting.pptxAbhijithKS36
The slide contains details of most common defects and troubleshooting(reason, causes, remedy) of polymer extruders used in industries for various types of polymer product manufacturing.
Mumbai University
Mechanical engineering
SEM III
Material Technology
Module 1.4
Strain Hardening:
Definition importance of strain hardening, Dislocation theory of strain hardening, Effect of strain hardening on engineering behaviour of materials, Recrystallization Annealing: stages of recrystallization annealing and factors affecting it
The document discusses three microstructural transformations: recovery, recrystallization, and grain growth that occur during annealing of cold worked materials. Recovery involves a reduction in point defects and dislocation rearrangement into low energy configurations at low annealing temperatures. Recrystallization occurs at higher annealing temperatures and results in the formation of new strain-free grains. Grain growth follows recrystallization and leads to an increase in the average grain size as larger grains grow at the expense of smaller ones.
1. The document discusses fatigue, which is structural damage that occurs when a material is subjected to cyclic loading below its tensile strength.
2. It describes how fatigue occurs through repeated loading and unloading causing microscopic cracks, and how factors like stress concentration, material properties, and the environment affect fatigue life.
3. The document outlines an experiment to determine the fatigue life of aluminum specimens under different stress levels using a fatigue testing machine. Results are analyzed to find the safe stress level for 1 million reversals.
It is a near net shape process in which casting and forging is done in single step.
It is Referred by many names such as “squeeze casting” , “pressure infiltration”, “liquid metal forging”, “extrusion casting”, “liquid pressing'', “pressure crystallization”.
The document presents a study on fabricating and characterizing an aluminum metal matrix composite reinforced with silicon carbide particles. The objectives are to fabricate the Al-SiC MMC, characterize its tensile strength and hardness properties, and determine optimal machining parameters for good surface finish. It discusses the composite materials, matrix, reinforcement, classification of composites, and metal matrix composites. It also details the properties of aluminum, silicon carbide, and aluminum silicon carbide composites. Methods of fabricating Al-SiC MMC including stir casting and characteristics like tensile testing, hardness testing, and machining tests are explained. Relevant literature on improving mechanical properties of Al-SiC composites is reviewed.
Flexibility Analysis In Industrial Piping Through The Finite Elements And Pho...IJERA Editor
This document analyzes the flexibility of industrial piping through finite element analysis, photoelasticity, and mathematical modeling. It presents the equations and properties used in each modeling method. The finite element model in ANSYS showed stress distributions that matched the mathematical model. The photoelasticity model allowed visualizing stress curves but values were difficult to obtain. The computational finite element model was determined to be best for industrial applications by providing reliable stress and deformation values and allowing complex analyses.
IRJET-Finite Element Analysis of Seat Belt Buckle AssemblyIRJET Journal
This study analyzed a seat belt buckle assembly using finite element analysis to determine the total deformation and von Mises stress under different loading conditions and thickness variations. A 3D model of the seat belt buckle was created in Solid Edge and meshed. The assembly was analyzed for loads of 63.5N to 350N and thicknesses of 8mm to 4mm. Results showed that total deformation and stress increased as thickness decreased, with a maximum deformation of 0.00125mm and maximum stress of 32.87MPa. The buckle's ultimate strength is 300MPa, so stresses remained well below the failure point. Thinner designs reduced material usage while maintaining structural integrity.
Rapid Fabrication of Nylon Surgical Sutures by 3D Printingjournal ijrtem
Abstract : Non-absorbable sutures such as monofilament nylon sutures are widely used in surgical treatments. These monofilament nylon sutures are fabricated by complicated extrusion process. In this study, a 3D printer is used for the first time to produce monofilament nylon suture, which could be used for eyes surgeries and others applications. Sutures fabricated in this study have diameter various from 60 to 100 μm, with capability of holding up to 4N load, which is comparable to the ones manufactured from conventional monofilament extrusion process. Keywords: 3D printing, monofilament suture, rapid prototyping
A critical comparison of shear tests for adhesive joints.pdfssuser9f67f31
This document summarizes and compares four methods for testing the shear strength of adhesive joints: single lap shear test (SLJ), thick adherent shear test (TAST), ARCAN test, and napkin ring test. It analyzes each method based on the stress and strain distributions within the joint, and the triaxiality ratio of normal to shear stresses, using analytical calculations and finite element modeling. The goal is to determine an optimal test configuration by understanding the advantages and limitations of each method for characterizing the mechanical behavior and fatigue properties of adhesive joints.
BEHAVIOR OF CONCRETE WITH PARTIAL REPLACEMENT OF C- AGGREGATES BY GRANULATED ...IRJET Journal
This document summarizes a study on the behavior of concrete with partial replacement of coarse aggregates by granulated rubber. Tests were performed on M25 grade concrete with 0%, 2.5%, 5%, 7.5%, 10%, 12.5%, and 15% replacement of coarse aggregates by rubber aggregates, with and without a superplasticizer. Compression, split tensile, and flexural tests were conducted on cubes, cylinders, and beams at 7 and 28 days. The results showed replacement of up to 7.5% rubber aggregates is permissible, with higher replacements resulting in decreased strength. Therefore, partial replacement of coarse aggregates with granulated rubber up to 7.5% is feasible.
This document summarizes research on creating highly sensitive and flexible strain gauges using carbon nanotube doped silver nano-ink printed on a flexible polyimide substrate with surrounding layers of polydimethylsiloxane (PDMS) elastomer. Testing showed that surrounding the strain gauge circuit with PDMS dramatically increased its sensitivity, with average gauge factors of 406.2 under tension and -232.6 under compression. Higher concentrations of carbon nanotubes in the silver nano-ink also improved sensitivity. The flexible and scalable manufacturing process has potential for applications requiring large-scale strain sensing like structural health monitoring.
This document summarizes research conducted on the failure of an 8000-ton heavy duty press. The researchers created a 3D model of the upper tool part and conducted finite element analysis to determine the stresses and strains. They found that low cycle fatigue was the mechanism responsible for failure of the upper tool part. Recommendations were made to stiffen the upper tool part to extend its life by reducing stresses. Submodeling and Neuber's approximation method were used to better understand stress distributions and strains in the upper tool part. The analyses identified low cycle fatigue as the cause of failure and provided suggestions to strengthen the tool and prolong its useful life.
The document describes a study on the effect of holes on the tensile strength of composite materials created through hand layup. It outlines the goals to develop a hand layup procedure and test how holes influence composite strength. The methodology section explains the hand layup process and sample preparation/testing. Results show the material's properties are lower than expected and holes reduce strength. The characteristic length, over which stresses average around a hole, is calculated to be approximately 0.133 inches.
Wear occurs to the hardest of materials, including diamond, wear studies having focused on surface damage in terms of material removal mechanisms, including transfer film, The wear testing rig is a device to simulate wears in the laboratory. The present work is about a design and manufacturing process of a pin on disk apparatus which is used as a test method for determining the wear of any two sliding materials. The aim of this paper is to give information about the design steps and manufacturing procedure for the pin on disk apparatus and to discuss the problems follows the design and manufacturing process. Km Sneha Soni | Abhishek Kumar | Adarsh Kumar Srivastav | Krishnanad Yadav | Mr. Rakesh Kumar Yadav "Fabrication of Pin-on-Disc Wear Test Rig" Published in International Journal of Trend in Scientific Research and Development (ijtsrd), ISSN: 2456-6470, Volume-4 | Issue-4 , June 2020, URL: https://www.ijtsrd.com/papers/ijtsrd30917.pdf Paper Url :https://www.ijtsrd.com/engineering/mechanical-engineering/30917/fabrication-of-pinondisc-wear-test-rig/km-sneha-soni
Finite Element Analysis of Damping Performance of VEM Materials Using CLD Tec...IJERA Editor
Most engineering structures experiences vibrational motion, this unwanted vibrations can result in premature
structural failure. Many methods are developed which enhances capability of damping such as constrained layer
damping. Shear motion is produced in VEM due to constraining layer to resist unwanted vibrational energy.
This paper shows theeffect of varying the thickness of viscoelastic materials on damping performance of CLD
beam.The damping performance is measured in terms of modal loss factor.
This document describes a photoelastic stress analysis of the bending strength of a helical gear. The analysis involved creating a 3D photoelastic model of the gear, subjecting it to loading, and freezing the stresses. Slices were cut from the model and observed under polarized light to determine stress distributions. Maximum bending stresses were calculated for different slices and scaled up to prototype values. Finite element analysis was also performed and showed good agreement with experimental results, with less than 2% variation in maximum stress values. The analysis found that helical gears experience higher peak bending stresses than spur gears due to their point contact loading.
The document is a lab report that tests different layups of carbon fiber reinforced epoxy composites to verify the 10% Rule of Mixtures. Four composite samples with layups of [0]8s, [90]8s, [+/-45]4s, and [0 90 +45 -45]2s were tested under 3-point bending and tension. The results found that the Rule of Mixtures accurately predicted the composite strengths and was generally conservative. The report concludes that the Rule of Mixtures allows fast prediction of composite performance for design requirements.
Modelling and Analysis of Hybrid Composite Joint Using Fem in AnsysIOSR Journals
Abstract: Composite materials are widely used in the various Fields. Due to the high strength they are widely
used in the low weight constructions and also used as a suitable alternative to metals. In various applications
and also for joining various composite parts together, they are fastened together using adhesives or Mechanical
fasteners. Modeling and static analysis of 3-D Models of joints such as bonded, riveted and hybrid. The results
were found in terms of vonmises stress, shear stress, and normal stress for stress distribution. ANSYS FEA tool
has been used for stress distribution characteristics of various configurations of double riveted single lap joint
with three joining methods namely bonded, riveted and hybrid the present study deals with the analysis of single
lap joint subjected to the given tensile load and the stress distribution in the members under various design
conditions are found.
This document provides a literature review and summary of finite element modeling of polymer nanocomposite adhesives. It reviews 10 papers on experimental and modeling studies of adhesive bonds. The document identifies gaps in research on shear strength estimation and limited exploration of adherend materials. The objective is to develop a 2D finite element model of a single-lap adhesive joint to analyze the effects of nanoparticle-filled adhesive on joint strength. The summary provides essential information on the topic, literature reviewed, research gaps identified and objective of further study.
This lab report summarizes a compression test experiment conducted to determine the mechanical properties of a metal alloy sample. The experiment involved compressing the sample between two plates using a universal testing machine while measuring stress and strain. The results showed the stress-strain curve for the material and identified its maximum compression strength. The objective was to learn how materials behave under compressive loads and determine properties like elastic modulus, yield point, and ultimate strength.
This lab report summarizes a compression test experiment conducted to determine the mechanical properties of a metal alloy sample. The experiment involved compressing the sample between two plates using a universal testing machine while measuring stress and strain. The results showed the stress-strain curve for the material and identified its maximum compression strength. The objective was to learn how materials behave under compressive loads and determine properties like elastic modulus, yield point, and ultimate strength.
In this lab, students tested the shear strength of two adhesives - cyanoacrylate and epoxy - using a testing machine. The maximum shear stress of each adhesive was calculated from the test data. Confidence intervals were also constructed for the shear stress results. The lab values were smaller than literature values, likely due to differences in specimen preparation between a student lab and professional testing. Epoxy was found to have a higher shear strength than cyanoacrylate based on the results.
All of material inside is un-licence, kindly use it for educational only but please do not to commercialize it.
Based on 'ilman nafi'an, hopefully this file beneficially for you.
Thank you.
A Review Paper on “Stress Analysis of Leaf Spring by using Photo Elasticity T...IRJET Journal
This document summarizes a review paper on analyzing leaf springs using photoelasticity techniques. It begins with an abstract discussing how leaf springs are commonly used in vehicle suspension systems and subjected to stress cycles that can lead to failure. Previous research has looked to improve leaf spring performance through new designs and materials. The review paper examines several papers on leaf spring design, analysis, fatigue life prediction, and failure analysis. It also discusses analyzing leaf springs using finite element analysis software. Photoelasticity is introduced as a nondestructive testing method to analyze stress distributions in complex geometries using the birefringent properties of certain materials when under load.
Effect of lamination angle on maximum deflection of simply supported composit...RAVI KUMAR
In this project a composite laminated beam is studied with glass-epoxy and graphite-epoxy combination. The beam is composed of four layers of different combination of composite material (glass epoxy and graphite epoxy composite). The beam is simply supported at both the ends and is subjected to uniformly distributed load along the length. Transverse deflection is computed for different lamination angle (0^0-〖90〗^0) by using Euler- Bernoulli’s theory (or CLPT). Maximum transverse deflection analysis is carried out using derived analytical expressions. The research carried out in this project will enable to determine the beam strength due to bending loads. The importance of fibre reinforcement in the manufacturing of the beam is studied in terms of bending strength of the beam. MATLAB codes are generated to implement analytical expiations of the composite beam.
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.
Similar to Diffuse and localized necking under plane stress in visco-plastic material models (20)
Expanding Access to Affordable At-Home EV Charging by Vanessa WarheitForth
Vanessa Warheit, Co-Founder of EV Charging for All, gave this presentation at the Forth Addressing The Challenges of Charging at Multi-Family Housing webinar on June 11, 2024.
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Diffuse and localized necking under plane stress in visco-plastic material models
1. 1
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
1
Paul Du Bois1
, Marcus Feucht2
, Salvatore Scalera3
1) Consultant, Freiligrahstr. 6, 63071 Offenburg, Germany
2) Daimler AG, EP/SPB, 71059 Sindelfingen, Germany
markus.feucht@daimler.com
3) DYNAmore Italia S.r.l., Piazza Castello, 139, 10124 Turin, Italy
salvatore.scalera@dynamore.de
Diffuse and localized necking under
plane stress in visco-plastic material
models
2. 2
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
ABSTRACTIn a tension test on a ductile material, a diffuse necking - so called because its spatial extension is
much larger than the sheet thickness - begins to develop in the sample when the strain hardening is
no longer able to compensate for the weakening due to the reduction of the cross section. After
some elongation under decreasing load, a localized neck usually appears in the region of the diffuse
neck. In the localized neck, severe thinning occurs leading to ultimate failure.
This work focuses on studying the diffuse and localized necking under plane stress conditions in
visco-plastic materials under dynamic loading. By means of a DOE analysis the main material
parameters that influence the occurrence of local and diffuse necking were determined. A material
model is then validated by systematic comparison of simulation results with physical tests carried
out at different strain rates. One methodology to achieve good correlation between test and
experiments is the use of a damage model. The damage model chosen by the authors is GISSMO
(Generalized Incremental Stress-State dependent damage Model), due to its widespread usage in the
crash community.
The GISSMO model is defined in terms of a critical plastic strain that indicates the start of damage
coupling and a failure plastic strain indicating fracture, both are defined as a function of stress
triaxiality. As the necking or more generally plastic instability will result in mesh dependency of the
simulation results, regularization is introduced by defining both the failure plastic strain and the
damage exponent as a function of the mesh size. As the spatial extension of the diffuse neck differs
as a function of strain rate, one way to achieve correlation between test and simulation is to express
these parameters as function of both the mesh size and the strain rate.
As consequence of the findings of this study, a number of new options were developed in the
GISSMO model.
3. 3
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
OVERVIEW
• INTRODUCTION
– Definition of diffuse & local necking and failure
– Failure models available in LS-DYNA. Why GISSMO?
• Visco-plastic material model
– Diffuse necking: new mathematical condition and its validation
– Local necking: DOE analysis to understand the influence of numerical
and phisical parameters
• GISSMO: short description
– Damage evolution
– Regularization
– Parameters identification
• GISSMO extension to include viscosity
– Description
– Correlation
• Conclusion
4. 4
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Notions in failure and instability theories
• Diffuse necking: the point where we
observe a loss of the homogeneous
state of deformation, a pretty CLEAR
notion, at least at a simulation level
• Local necking: basically the formability
limit, a rather FUZZY notion that needs
to be defined for every application, can
depend on the size of imperfection and
the size of the grid (numerical). To
better understand this phenomena, a
DOE analysis was carried out. The
results will be discussed further in this
presentation.
• Failure: the point where a simply
connected part becomes multiply
connected: cracks appear, also a pretty
CLEAR notion
introduction diffuse necking local necking failure
5. 5
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Some failure models in LS-DYNA. Why GISSMO?
• GISSMO is a simple yet powerful damage and failure concept within LS-DYNA developed at Daimler in
cooperation with DYNAmore. Currently it is used and evaluated in most automotive companies (and
even copied by other codes).
• It is based on the Johnson-Cook approach but generalized to suite various crash and metal forming
demands.
• It can be used a simple failure criteria or a rather complex damage and failure model. Hence it can be
coupled to stresses and act as damage model.
• It might be used in sheet metal forming and crashworthiness and in both applications to close the gap
between forming and crashworthiness simulations.
• Existing Material Models are kept unaltered (usually MAT24 for crash)
introduction diffuse necking local necking failure
6. 6
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Visco-plastic material: diffuse necking
𝐸𝑡 𝜖 + η 𝜀, 𝜀
𝜀
𝜀
≥ 𝜎 𝐸𝑡 =
𝜕𝜎
𝜕𝜀
η =
𝜕𝜎
𝜕𝜀
• Material model 1 (MAT24 tabulated)
𝜎 𝜎
𝜀 𝜀Observation:
• the uni-axial tensile test, carried out using a specimen characterized by the
material described above, gives ambiguous output also in the case of a simply
elasto-plastic behaviour.
• Considering two different material – both without strain-rate dependency - with
Et1 Et2, the shape of the necking point is completely different.
Conclusion:
The hypotesis of linear bahavior of the stress has to be removed
introduction diffuse necking local necking failure
The equation was written starting from the algorithmic expression of the stress increment,
combined with the condition of instability for having the necking point
7. 7
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
𝐸𝑡 𝜖 + η 𝜀, 𝜀
𝜀
𝜀
≥ 𝜎 → 𝑛 ∗ 𝑏 ∗ 𝜀 𝑛−1
+
η ∗ 𝜀
𝜀
𝜎 = 𝑎 + 𝑏 ∗ 𝜖 𝑛
→ 𝐸𝑡 =
𝑑𝜎
𝑑𝜀
= 𝑛 ∗ 𝑏 ∗ 𝜀 𝑛−1
𝜎
𝜎
• Material model 2 (MAT24 tabulated)
Observation:
• Also in this case, a preliminary investigation only considering the
elasto-plastic behaviour, was conducted. As expected, the
condition for the localization
𝑑𝜎
𝑑𝜀
= 𝜎 is accurately verified and the
extension of the necking point is confined to the centre of the
specimen like in the quasi-static physical tests.
• The simulated tests conducted with the the visco-plastic material
shows again a 𝑑 ≫ 𝑑0, the longitudinal extension of the neck is
much grater than the one commonly observed in real dynamical
tests conducted on different type of steels
Conclusion:
The hypothesis of linear behaviour of the stress as function of the
strain rate has to be removed. In other terms
𝑑 = 𝑑 𝐸𝑡 𝜖 , η 𝜀, 𝜀
𝜀
𝜀
introduction diffuse necking local necking failure
9. 9
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
• Material model 3 (MAT24 tabulated)
Observation:
• Assigning to the constants, the following set of the values
𝜎1 = 0.5 𝜎2 = 0.7 𝑏 = 0.8 𝑛 = 0.5 𝜀1 = 1𝑒−4
𝜀2 = 0.1,
the condition of no necking assumes the simplified formula:
𝐸𝑡 𝜖 + η 𝜀, 𝜀
𝜀
𝜀
≥ 𝜎 → 𝑛 ∗ 𝑏 ∗ 𝜀 𝑛−1
+
𝜀
𝜀2 ∗
𝜎2−𝜎1
ln 𝜀2 −ln 𝜀1
≥ 𝜎
0.4
𝜖
+ 0.03
𝜀
𝜀2 ≥ 𝜎
Conclusion:
When 𝑑𝐹 = 0 →
0.4
𝜖
+ 0.03
𝜀
𝜀2 = 𝜎; the new local condition of no necking for visco-
plastic material is confirmed by this experience.
𝜎 𝐹
𝑡 𝑡
introduction diffuse necking local necking failure
10. 10
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
The local condition
𝐸𝑡 𝜖 = 𝜎 elasto-plastic material
𝐸𝑡 𝜖 + η 𝜀, 𝜀
𝜀
𝜀
≥ 𝜎 visco-plasti material
is able to predict when the instability occurs, but of
course it can’t describe the instability itself.
Visco-plastic material: brittle & ductile behaviour
From that moment on, a diffuse neck begins to develop
in the sample because the strain hardening is not able
to compensate anymore the weakening due to the
reduction in width and thickness of the cross section.
After some elongation under decreasing load, a
localized neck suddenly appears in the region of the
diffuse neck. In the localized neck, mainly thinning
occurs
11. 11
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
• Material model 4 (MAT 24 C&S)
Visco-plastic material: local neckingTo identify which are the factors that influence the local necking, or in other terms, that lead to a brittle or ductile
behaviour of the material, a DOE analysis was carried out.
The material model is a piecewise liner plasticity and the strain rate is accounted for, using the Cowper and
Symonds model:
𝜎 = 𝑎 + 𝑏 ∗ 𝜀 𝑛
∗ 1 +
𝜀
𝐶
1
𝑝
𝜎
𝜀
nominal Max Min
a 0.4 0.5 0.7
b 0.8 0 1
n 0.5 0 1
C 150 40 6500
p 3 2 10
Target of the DOE analysis: identify the parameters
which have major influence on the diffuse necking
introduction diffuse necking local necking failure
12. 12
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Main results of the DOE analysis
introduction diffuse necking local necking failure
13. 13
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
introduction diffuse necking local necking failure
a=0.5
C= 40
p=5
Main results of the DOE analysis
𝜎 = 𝑎 + 𝑏 ∗ 𝜀 𝑛
∗ 1 +
𝜀
𝐶
1
𝑝
14. 14
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Failure model: the philosophy of GISSMO
• The user defines a failure curve (the
onset of cracks) and a critical strain
curve (the loss of uniformity in the
strain field)
• Between the critical strain curve and
the failure curve, we assume a
continuous process of localization,
inducing mesh dependency.
introduction diffuse necking local necking failure
15. 15
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Failure model: the philosophy of GISSMO
introduction diffuse necking local necking failure
16. 16
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Regularization in GISSMO
introduction diffuse necking local necking failure
17. 17
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Extension of GISSMO to visco-plasticity
engineeringstress
REGULARIZATION
engineering strain
CORRELATION
New extension of LS-DYNA: strain rate dependecies for
fade exponent and regularization factor
introduction diffuse necking local necking failure
18. 18
9th European LS-DYNA User‘s Conference – Manchester - 2-4. June 2013
Acknowledgements
• Diffuse necking, local necking, failure were discussed for
visco-plastic material
• Diffuse necking: new condition with a preliminary validation
of the mathematical model. Further investigation needed
• Local necking: DOE analysis to start a numerical interpretation
of such fuzzy phenomena
• Failure: GISSMO extension
• Correlation with experimental tests
Conclusions
Thanks to Dr. Tobias Erhart for implementing the extensions in LS-DYNA and to Dr.
Andre Haufe, Dr. Tobias Graf and Dr. Filipe Andrade for their active collaboration in the
understanding and interpretation of the physical phenomena emerging from the real
and the virtual tests.