The document discusses various theories of material failure including maximum principal stress, maximum shear stress, maximum principal strain, maximum strain energy density, and maximum distortion energy density. It provides brief explanations of each theory, noting that maximum principal stress is good for brittle materials, maximum shear stress and maximum distortion energy density are good for ductile materials, and recommends the maximum distortion energy density theory.
The document discusses various theories of failure that are used to determine the safe dimensions of components under combined loading conditions. It describes five theories: (1) Maximum principal stress theory, (2) Maximum principal strain theory, (3) Maximum strain energy theory, (4) Maximum distortion energy theory, and (5) Maximum shear stress theory. The maximum distortion energy theory provides the safest design for ductile materials as it results in the largest allowable stresses before failure compared to the other theories. The document also compares the various theories and discusses when each is best applied depending on the material type and stress conditions.
The document discusses different theories of material failure including maximum principal stress, maximum shear stress, maximum principal strain, maximum strain energy, and maximum distortion energy theories. It provides details on each theory, noting that maximum principal stress theory is suitable for brittle materials, maximum shear stress theory for ductile materials, and maximum distortion energy theory is highly recommended.
This document discusses static failure theories for analyzing machine components under loading. It begins by asking why parts fail and explaining that failure depends on the material properties and type of loading. It then covers different failure modes and the need for separate theories for ductile and brittle materials. The key static failure theories presented are maximum normal stress theory, maximum shear stress theory, distortion energy theory, and their applications to ductile and brittle materials. Examples are provided to illustrate Mohr's circle analysis and applying the theories.
1. The document discusses four common failure theories used in engineering: maximum shear stress theory, maximum principal stress theory, maximum normal strain theory, and maximum shear strain theory.
2. It provides details on the maximum shear stress (Tresca) theory, which states that failure occurs when the maximum shear stress equals the yield point stress under simple tension.
3. An example problem is presented involving determining the required diameter of a circular shaft using the maximum shear stress theory with a safety factor of 3, given the material properties and loads on the shaft.
1. There are five main theories of failure used to predict failure of machine components under multi-axial stresses: Rankine, Tresca, Saint Venant, Haigh, and Hencky-Von Mises.
2. Theories of failure are required because material strengths are determined from uni-axial tests, while actual components experience multi-axial stresses, and the theories relate uni-axial strengths to multi-axial stresses.
3. Rankine's theory applies to brittle materials and ductile materials under uniaxial or similar biaxial stresses, while Tresca's theory applies to ductile materials prone to shear failure.
This document provides an overview of fatigue in metals. It discusses stress cycles and the S-N curve used to represent fatigue data. The effects of mean stress, stress range, and stress concentration on fatigue properties are examined. Low cycle fatigue involving high strains is also covered. The document introduces approaches for assessing fatigue properties, including the cyclic stress-strain curve and fatigue crack growth resistance. Factors that influence fatigue such as temperature are also discussed.
The document discusses stress concentration and fatigue failure in machine elements. It defines stress concentration as the localization of high stresses due to irregularities or abrupt changes in cross-section. Stress concentration can be reduced by avoiding sharp changes in cross-section and providing fillets and chamfers. Fatigue failure occurs when fluctuating stresses cause cracks over numerous load cycles. The endurance limit is the maximum stress amplitude that causes failure after an infinite number of cycles. Factors like stress concentration, surface finish, size, and mean stress affect the endurance limit. Designs should minimize stress raisers and protect against corrosion to prevent fatigue failures.
The document discusses various theories of material failure including maximum principal stress, maximum shear stress, maximum principal strain, maximum strain energy density, and maximum distortion energy density. It provides brief explanations of each theory, noting that maximum principal stress is good for brittle materials, maximum shear stress and maximum distortion energy density are good for ductile materials, and recommends the maximum distortion energy density theory.
The document discusses various theories of failure that are used to determine the safe dimensions of components under combined loading conditions. It describes five theories: (1) Maximum principal stress theory, (2) Maximum principal strain theory, (3) Maximum strain energy theory, (4) Maximum distortion energy theory, and (5) Maximum shear stress theory. The maximum distortion energy theory provides the safest design for ductile materials as it results in the largest allowable stresses before failure compared to the other theories. The document also compares the various theories and discusses when each is best applied depending on the material type and stress conditions.
The document discusses different theories of material failure including maximum principal stress, maximum shear stress, maximum principal strain, maximum strain energy, and maximum distortion energy theories. It provides details on each theory, noting that maximum principal stress theory is suitable for brittle materials, maximum shear stress theory for ductile materials, and maximum distortion energy theory is highly recommended.
This document discusses static failure theories for analyzing machine components under loading. It begins by asking why parts fail and explaining that failure depends on the material properties and type of loading. It then covers different failure modes and the need for separate theories for ductile and brittle materials. The key static failure theories presented are maximum normal stress theory, maximum shear stress theory, distortion energy theory, and their applications to ductile and brittle materials. Examples are provided to illustrate Mohr's circle analysis and applying the theories.
1. The document discusses four common failure theories used in engineering: maximum shear stress theory, maximum principal stress theory, maximum normal strain theory, and maximum shear strain theory.
2. It provides details on the maximum shear stress (Tresca) theory, which states that failure occurs when the maximum shear stress equals the yield point stress under simple tension.
3. An example problem is presented involving determining the required diameter of a circular shaft using the maximum shear stress theory with a safety factor of 3, given the material properties and loads on the shaft.
1. There are five main theories of failure used to predict failure of machine components under multi-axial stresses: Rankine, Tresca, Saint Venant, Haigh, and Hencky-Von Mises.
2. Theories of failure are required because material strengths are determined from uni-axial tests, while actual components experience multi-axial stresses, and the theories relate uni-axial strengths to multi-axial stresses.
3. Rankine's theory applies to brittle materials and ductile materials under uniaxial or similar biaxial stresses, while Tresca's theory applies to ductile materials prone to shear failure.
This document provides an overview of fatigue in metals. It discusses stress cycles and the S-N curve used to represent fatigue data. The effects of mean stress, stress range, and stress concentration on fatigue properties are examined. Low cycle fatigue involving high strains is also covered. The document introduces approaches for assessing fatigue properties, including the cyclic stress-strain curve and fatigue crack growth resistance. Factors that influence fatigue such as temperature are also discussed.
The document discusses stress concentration and fatigue failure in machine elements. It defines stress concentration as the localization of high stresses due to irregularities or abrupt changes in cross-section. Stress concentration can be reduced by avoiding sharp changes in cross-section and providing fillets and chamfers. Fatigue failure occurs when fluctuating stresses cause cracks over numerous load cycles. The endurance limit is the maximum stress amplitude that causes failure after an infinite number of cycles. Factors like stress concentration, surface finish, size, and mean stress affect the endurance limit. Designs should minimize stress raisers and protect against corrosion to prevent fatigue failures.
Saint-Venant's principle states that the stresses and strains far away from the load application point are unaffected by the exact nature of the load or its application method, but only depend on the resultant load magnitude and application area. Stress concentrations occur where the cross-sectional area changes abruptly, like holes, notches, or threads, and cause local stress values much higher than the average stress. The stress concentration factor K is used to relate the maximum stress σmax to the average stress σave in a cross-section. Design engineers use stress concentration factors and allowable stress values to determine if a given load will exceed the material's strength at stress concentration locations.
Maximum principal stress theory.
Maximum shear stress theory.
Maximum shear strain theory.
Maximum strain energy theory.
Maximum shear strain energy theory.
This document provides an introduction to machine design and its various considerations. It defines machine design as the process of engineering design that involves designing machine elements and arranging them optimally to obtain useful work. Some key points covered include:
- Classification of machine design types including adaptive, development, and new design.
- Factors to consider in machine design such as material selection, forces on elements, size, shape, weight, manufacturing method, reliability, and cost.
- The general procedure of machine design including need identification, mechanism synthesis, force analysis, material selection, element design, modification, and drawing production.
- Considerations for manufacturability such as reducing part counts, modular design, and designing for
This document provides an introduction to fatigue, including:
- Fatigue occurs when a component is subjected to fluctuating stresses and fails at a stress lower than its static strength.
- It accounts for 90% of mechanical failures and occurs suddenly without warning.
- Three factors are needed for fatigue failure: a maximum stress, stress variation, and sufficient number of cycles.
- Fatigue testing involves subjecting specimens to cyclic stresses and recording the number of cycles until failure to generate an S-N curve.
The document discusses various topics related to stress and strain including: principal stresses and strains, Mohr's stress circle theory of failure, 3D stress and strain, equilibrium equations, and impact loading. It provides examples of stresses acting in different planes including normal, shear, oblique, and principal planes. It also gives examples of calculating normal and tangential stresses on an oblique plane subjected to stresses in one, two, or multiple directions with and without shear stresses.
This document discusses the course MDPN452 Mechanics of Composite Materials, taught by Dr. Mohammad Tawfik. It covers topics related to micromechanics of composites including the relationship between composite and constituent material properties, designing composites to achieve desired stiffness and strength, assumptions of micromechanics models, approaches to determining elastic properties like stiffness and Poisson's ratio, and models for predicting strength in tension and compression. Students are assigned homework to research models of tensile and compressive failure in composites and compare them to experimental data.
Stress concentration occurs where there are irregularities or discontinuities in a material, like holes or grooves, and greatly increases stresses in these local areas, where fatigue failure often originates. Stress concentration factors quantify how much a discontinuity increases stresses but are not needed for ductile materials under static loads, as local yielding relieves these concentrations. Notch sensitivity values between 0 and 1 indicate a material's sensitivity to notches, with 1 being fully sensitive and 0 having no sensitivity. Geometric stress concentration factors estimate stress amplification near geometric features.
1. The document defines static load, failure, material strength properties including yield strength and ultimate strength in tension and compression.
2. It describes ductile materials as deforming significantly before fracturing, while brittle materials yield very little before fracturing and have similar yield and ultimate strengths.
3. The maximum shear stress theory and distortion energy theory are introduced as failure theories used in design based on yield strength and ultimate strength respectively. Safety factors are used to avoid failure based on these theories.
Design against fluctuating loads, stress concentration, Goodman and Modified Goodman Diagrams, Factors affecting stress concentration, Use of charts for finding stress concentration facotrs
This document summarizes key concepts about columns and struts. It defines struts as structural members under axial compression, while columns are vertical struts. Columns can be short or long depending on their length-to-minimum radius of gyration ratio. Euler's formula and Rankine's formula provide methods to calculate the buckling/crippling load of columns based on factors like the modulus of elasticity, moment of inertia, and effective length. The document also discusses radius of gyration, slenderness ratio, crushing load, and how eccentric loading affects column stresses.
1. The document discusses the dynamics of machines and introduces the key concepts of kinematics, dynamics, kinetics, and statics as the four main branches of the theory of machines.
2. It then discusses static and dynamic force analysis and introduces concepts like inertia forces and torques. D'Alembert's principle is explained which states that inertia and external forces together result in static equilibrium.
3. Methods for dynamic analysis of reciprocating engines like graphical and analytical methods are introduced. Key forces on reciprocating parts like piston effort, connecting rod force, thrust, crank pin effort, and crank effort are defined.
This document discusses machine design and the basic procedures and requirements for designing machine elements. It defines machine design as using scientific principles, technical information, and imagination to describe machines that perform functions with maximum economy and efficiency. The basic requirements for machine elements are then listed, including strength, rigidity, wear resistance, manufacturability, safety, and more. The basic procedure for designing machine elements is then outlined in 6 steps: specification of function, determination of forces, selection of material, failure criterion, determination of dimensions, and preparation of working drawings. Materials that could be used like cast iron, plain carbon steel, and alloy steels are then described in more detail.
The document discusses stress concentration and fatigue failure in machine elements. It defines stress concentration as irregular stress distribution caused by abrupt changes in cross-section shape. Stress concentration factors are introduced to quantify the maximum stress compared to nominal stress. The document also discusses endurance limit and fatigue strength testing methods. Factors that affect fatigue strength like material properties, surface finish, size and temperature are summarized. Methods to evaluate and reduce stress concentration in designs are provided.
The document discusses different types of welded joints used in mechanical assemblies, including butt joints, fillet/lap joints, transverse fillet welds, and parallel fillet welds. It provides formulas to calculate the strength of different welded joint configurations based on factors like weld throat area, plate dimensions, and allowable tensile and shear stresses. Examples are given to demonstrate calculating the required weld lengths for specific plate joining problems based on the given stresses and loads.
The document discusses riveted joints. It describes the different types of rivets and rivet heads. The key types of riveted joints are lap joints and butt joints. Important terms used in riveted joints are also defined, such as pitch and margin. Guidelines for the proportions of dimensions for riveted joints are provided. Examples of different double and single riveted lap and butt joints are shown.
Unit 2 Design Of Shafts Keys and CouplingsMahesh Shinde
This document provides information about the design of shafts, keys, and couplings. It discusses transmission shafts, stresses induced in shafts, and shaft design based on strength and rigidity. It presents formulas for shaft design using maximum shear stress theory, distortion energy theory, and the ASME code. Several examples are provided to demonstrate how to calculate the diameter of a shaft given the power transmitted, loads on the shaft, material properties, and other parameters using these theories and codes. Assignments involving similar calculations of shaft diameters are presented.
The various forces acts on the reciprocating parts of an engine.
The resultant of all the forces acting on the body of the engine due to inertia forces only is known as unbalanced force or shaking force.
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.
UNIT-I-Theories of failures-19072016.pptxPraveen Kumar
The document discusses various theories of material failure under complex loading conditions, including:
1) Maximum principal stress theory (Rankine), which states failure occurs when the maximum principal stress equals the yield stress from a tensile test.
2) Maximum shear stress theory (Guest-Tresca), which states failure occurs when the maximum shear stress equals the shear stress from a tensile test.
3) Maximum principal strain theory (Saint-Venant), which states failure occurs when the maximum principal strain equals the yield strain from a tensile test.
4) Theories also consider total strain energy, maximum shear strain energy, and distortional strain energy.
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.
Saint-Venant's principle states that the stresses and strains far away from the load application point are unaffected by the exact nature of the load or its application method, but only depend on the resultant load magnitude and application area. Stress concentrations occur where the cross-sectional area changes abruptly, like holes, notches, or threads, and cause local stress values much higher than the average stress. The stress concentration factor K is used to relate the maximum stress σmax to the average stress σave in a cross-section. Design engineers use stress concentration factors and allowable stress values to determine if a given load will exceed the material's strength at stress concentration locations.
Maximum principal stress theory.
Maximum shear stress theory.
Maximum shear strain theory.
Maximum strain energy theory.
Maximum shear strain energy theory.
This document provides an introduction to machine design and its various considerations. It defines machine design as the process of engineering design that involves designing machine elements and arranging them optimally to obtain useful work. Some key points covered include:
- Classification of machine design types including adaptive, development, and new design.
- Factors to consider in machine design such as material selection, forces on elements, size, shape, weight, manufacturing method, reliability, and cost.
- The general procedure of machine design including need identification, mechanism synthesis, force analysis, material selection, element design, modification, and drawing production.
- Considerations for manufacturability such as reducing part counts, modular design, and designing for
This document provides an introduction to fatigue, including:
- Fatigue occurs when a component is subjected to fluctuating stresses and fails at a stress lower than its static strength.
- It accounts for 90% of mechanical failures and occurs suddenly without warning.
- Three factors are needed for fatigue failure: a maximum stress, stress variation, and sufficient number of cycles.
- Fatigue testing involves subjecting specimens to cyclic stresses and recording the number of cycles until failure to generate an S-N curve.
The document discusses various topics related to stress and strain including: principal stresses and strains, Mohr's stress circle theory of failure, 3D stress and strain, equilibrium equations, and impact loading. It provides examples of stresses acting in different planes including normal, shear, oblique, and principal planes. It also gives examples of calculating normal and tangential stresses on an oblique plane subjected to stresses in one, two, or multiple directions with and without shear stresses.
This document discusses the course MDPN452 Mechanics of Composite Materials, taught by Dr. Mohammad Tawfik. It covers topics related to micromechanics of composites including the relationship between composite and constituent material properties, designing composites to achieve desired stiffness and strength, assumptions of micromechanics models, approaches to determining elastic properties like stiffness and Poisson's ratio, and models for predicting strength in tension and compression. Students are assigned homework to research models of tensile and compressive failure in composites and compare them to experimental data.
Stress concentration occurs where there are irregularities or discontinuities in a material, like holes or grooves, and greatly increases stresses in these local areas, where fatigue failure often originates. Stress concentration factors quantify how much a discontinuity increases stresses but are not needed for ductile materials under static loads, as local yielding relieves these concentrations. Notch sensitivity values between 0 and 1 indicate a material's sensitivity to notches, with 1 being fully sensitive and 0 having no sensitivity. Geometric stress concentration factors estimate stress amplification near geometric features.
1. The document defines static load, failure, material strength properties including yield strength and ultimate strength in tension and compression.
2. It describes ductile materials as deforming significantly before fracturing, while brittle materials yield very little before fracturing and have similar yield and ultimate strengths.
3. The maximum shear stress theory and distortion energy theory are introduced as failure theories used in design based on yield strength and ultimate strength respectively. Safety factors are used to avoid failure based on these theories.
Design against fluctuating loads, stress concentration, Goodman and Modified Goodman Diagrams, Factors affecting stress concentration, Use of charts for finding stress concentration facotrs
This document summarizes key concepts about columns and struts. It defines struts as structural members under axial compression, while columns are vertical struts. Columns can be short or long depending on their length-to-minimum radius of gyration ratio. Euler's formula and Rankine's formula provide methods to calculate the buckling/crippling load of columns based on factors like the modulus of elasticity, moment of inertia, and effective length. The document also discusses radius of gyration, slenderness ratio, crushing load, and how eccentric loading affects column stresses.
1. The document discusses the dynamics of machines and introduces the key concepts of kinematics, dynamics, kinetics, and statics as the four main branches of the theory of machines.
2. It then discusses static and dynamic force analysis and introduces concepts like inertia forces and torques. D'Alembert's principle is explained which states that inertia and external forces together result in static equilibrium.
3. Methods for dynamic analysis of reciprocating engines like graphical and analytical methods are introduced. Key forces on reciprocating parts like piston effort, connecting rod force, thrust, crank pin effort, and crank effort are defined.
This document discusses machine design and the basic procedures and requirements for designing machine elements. It defines machine design as using scientific principles, technical information, and imagination to describe machines that perform functions with maximum economy and efficiency. The basic requirements for machine elements are then listed, including strength, rigidity, wear resistance, manufacturability, safety, and more. The basic procedure for designing machine elements is then outlined in 6 steps: specification of function, determination of forces, selection of material, failure criterion, determination of dimensions, and preparation of working drawings. Materials that could be used like cast iron, plain carbon steel, and alloy steels are then described in more detail.
The document discusses stress concentration and fatigue failure in machine elements. It defines stress concentration as irregular stress distribution caused by abrupt changes in cross-section shape. Stress concentration factors are introduced to quantify the maximum stress compared to nominal stress. The document also discusses endurance limit and fatigue strength testing methods. Factors that affect fatigue strength like material properties, surface finish, size and temperature are summarized. Methods to evaluate and reduce stress concentration in designs are provided.
The document discusses different types of welded joints used in mechanical assemblies, including butt joints, fillet/lap joints, transverse fillet welds, and parallel fillet welds. It provides formulas to calculate the strength of different welded joint configurations based on factors like weld throat area, plate dimensions, and allowable tensile and shear stresses. Examples are given to demonstrate calculating the required weld lengths for specific plate joining problems based on the given stresses and loads.
The document discusses riveted joints. It describes the different types of rivets and rivet heads. The key types of riveted joints are lap joints and butt joints. Important terms used in riveted joints are also defined, such as pitch and margin. Guidelines for the proportions of dimensions for riveted joints are provided. Examples of different double and single riveted lap and butt joints are shown.
Unit 2 Design Of Shafts Keys and CouplingsMahesh Shinde
This document provides information about the design of shafts, keys, and couplings. It discusses transmission shafts, stresses induced in shafts, and shaft design based on strength and rigidity. It presents formulas for shaft design using maximum shear stress theory, distortion energy theory, and the ASME code. Several examples are provided to demonstrate how to calculate the diameter of a shaft given the power transmitted, loads on the shaft, material properties, and other parameters using these theories and codes. Assignments involving similar calculations of shaft diameters are presented.
The various forces acts on the reciprocating parts of an engine.
The resultant of all the forces acting on the body of the engine due to inertia forces only is known as unbalanced force or shaking force.
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.
UNIT-I-Theories of failures-19072016.pptxPraveen Kumar
The document discusses various theories of material failure under complex loading conditions, including:
1) Maximum principal stress theory (Rankine), which states failure occurs when the maximum principal stress equals the yield stress from a tensile test.
2) Maximum shear stress theory (Guest-Tresca), which states failure occurs when the maximum shear stress equals the shear stress from a tensile test.
3) Maximum principal strain theory (Saint-Venant), which states failure occurs when the maximum principal strain equals the yield strain from a tensile test.
4) Theories also consider total strain energy, maximum shear strain energy, and distortional strain energy.
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.
The document discusses various failure theories for static loads on materials. It describes ductile and brittle materials, and the theories used to analyze failure for each type. For ductile materials, it covers maximum shear stress theory and distortion energy theory, including the von Mises yield criterion. It provides equations used in the theories and discusses applying a safety factor in design. For brittle materials, it presents the Modified Coulomb-Mohr theory and divides the failure envelope into three zones for design.
Elastic Strain Energy due to Gradual Loading.
Elastic Strain Energy due to Sudden Loading.
Elastic Strain energy due to impact loading.
Elastic Strain Energy due to Principal Stresses.
Energy of Dilation And Distortion.
This document discusses material properties and bending stresses. It defines key terms like modulus of elasticity, Poisson's ratio, yield stress, and ultimate tensile stress. It explains that plane sections remain plane after bending but rotate, and that the neutral axis experiences no deformation or stress. The location of the neutral axis depends on the material properties and loading conditions. Equations are provided to calculate bending stresses based on the neutral axis location and applied moment. An example problem calculates bending stresses at different points on an airplanes wing. The document also notes that for very high loads above the elastic range, stresses become nonlinear and the neutral axis must be determined through trial and error.
The document discusses five theories of failure - maximum normal stress, maximum normal strain, maximum shear stress, strain energy, and maximum distortion energy. The maximum normal stress and strain theories apply only to brittle materials, while the remaining three apply to ductile materials. Failure occurs when the stress or strain on a material reaches the ultimate stress or strain value from a tensile test. The theories provide ways to determine failure based on relationships between principal stresses or strains.
1) Mohr's circle is a graphical representation used to analyze stresses on planes at a point in a stressed body under plane stress conditions. It relates normal and shear stresses acting on inclined planes.
2) To construct Mohr's circle, the normal and shear stresses on the x and y faces of a sample are plotted on a stress diagram. A line is drawn between these points and extended to intersect the normal stress axis, establishing the center of the circle.
3) Mohr's circle allows visualization of relationships between stresses, including determining principal stresses, maximum shear stress, and planes on which they act from the circle's dimensions.
This document provides an overview of geomechanics concepts for petroleum engineers. It discusses stress and strain theory, elasticity, homogeneous and heterogeneous stress fields, principal stresses, and the Mohr circle construction. It also covers rock deformation mechanisms including cataclasis and intracrystalline plasticity. Key concepts are defined such as normal and shear stress, elastic moduli like Young's modulus and Poisson's ratio, elastic stress-strain equations, and strain measures including conventional, quadratic, and natural strain.
This summary provides the key details about four failure theories in 3 sentences:
The document discusses four common failure theories: 1) Maximum shear stress (Tresca) theory, which predicts failure when maximum shear stress equals yield stress, applies to ductile materials. 2) Maximum principal stress (Rankine) theory, which predicts failure when largest principal stress reaches ultimate stress. 3) Maximum normal strain (Saint Venant) theory, which predicts failure when maximum normal strain equals yield strain. 4) Maximum shear strain (distortion energy) theory, which predicts failure when distortion energy per unit volume equals strain energy at failure. The theories attempt to predict failure of materials subjected to multiaxial stress states.
The document discusses inelastic material behavior and yield criteria. It introduces nonlinear stress-strain relationships and various yield criteria models used for ductile and brittle materials, including maximum principal stress, Tresca shear stress, and von Mises distortional energy criteria. It also covers Hooke's law for isotropic elasticity and defines strain energy density. Key concepts discussed are nonlinear response, idealized stress-strain curves, general yield criteria concepts, and conditions for material yielding under multiaxial stress states.
This document discusses stress and strain concepts including:
1. Definitions of normal stress, normal strain, Poisson's ratio, shear stress, and shear strain. It also discusses tensile testing and stress-strain curves.
2. Stress-strain curves are shown for ductile and brittle materials. An example curve for low-carbon steel is described.
3. True stress and true strain are defined based on instantaneous cross-sectional area and gage length. Different regions of stress-strain curves are identified.
The document discusses plasticity theory and yield criteria. It introduces Hooke's law and its limitations under large strains. Generalized Hooke's law is presented for isotropic and anisotropic materials. Common stress-strain curves are shown including elastic-plastic and strain hardening responses. Several yield criteria are covered, including maximum principal stress, Tresca, and von Mises criteria. The von Mises criterion uses a second invariant of stress to predict yielding of ductile materials. An example compares predictions of yielding using Tresca and von Mises criteria for a given stress state in aluminum.
This document discusses key concepts in machine design and material stress including:
- Stress is defined as the internal resisting force per unit area when an external force is applied. Strain is the change in length per original length when a body experiences a force.
- There are two types of loads: static loads which do not vary over time, and dynamic loads where magnitude and direction vary over time, including cyclic and impact loads.
- Fatigue failure can occur when components fail under cyclic stress levels below the ultimate tensile strength due to repeated loading. The endurance limit is the maximum stress amplitude a material can withstand without failing.
- Failure theories like maximum principal stress and maximum shear stress theories define when failure
The document discusses different types of strain energy stored in materials when subjected to loads. It defines strain energy as the work done or energy stored in a body during elastic deformation. The types of strain energy discussed include: elastic strain energy, strain energy due to gradual, sudden, impact, shock and shear loading. Formulas are provided to calculate strain energy due to these different loadings. Examples of calculating strain energy in axially loaded bars and beams subjected to bending and torsional loads are also presented.
Mohamad Redhwan Abd Aziz is a lecturer at the DEAN CENTER OF HND STUDIES who teaches the subject of Solid Mechanics (BME 2023). The 3 credit hour course involves 2 hours of lectures and 2 hours of labs/tutorials each week. Student assessment includes quizzes, assignments, tests, lab reports, and a final exam. The course objectives are to understand stress, strain, and forces in solid bodies through various principles and experiments. Topic areas covered include stress and strain, elasticity, shear, torsion, bending, deflection, and more. References for the course are provided.
This document discusses different theories of failure due to static loading, including maximum normal stress theory, maximum shear stress theory, and distortion energy theory. It provides explanations of each theory, the conditions under which failure occurs according to each, and how to calculate the factor of safety. An example calculation is also given to demonstrate computing the factor of safety for different stress states according to each theory.
This document discusses different theories of failure due to static loading, including maximum normal stress theory, maximum shear stress theory, and distortion energy theory. It provides explanations of each theory, the conditions under which failure occurs according to each, and how to calculate the factor of safety. An example calculation is also shown applying the different failure theories to different stress states.
This document discusses different theories of failure due to static loading, including maximum normal stress theory, maximum shear stress theory, and distortion energy theory. It provides explanations of each theory, the conditions under which failure occurs according to each, and how to calculate the factor of safety. An example calculation is also shown applying the different failure theories to different stress states.
This document discusses vibration transmissibility and contains a summary of key concepts:
1) Transmissibility is defined as the ratio of the amplitude/force transmitted to the excitation amplitude/force. It measures the effectiveness of vibration isolation.
2) Force transmissibility (TR) is the ratio of the force transmitted to the supporting structure to the force impressed on the system.
3) The transmissibility (TR) of a damped forced vibration system is derived. TR depends on damping ratio (ξ), frequency ratio (r), and approaches zero as r approaches infinity.
4) Transmissibility curves plot TR versus frequency ratio under different damping conditions. They show TR tends to one at
Understanding optistruct & LS-Dyna files using text editorAkshay Mistri
This describes basic usage of a text editor in building, editing and organizing FEA model files. Using text editor allows user to do quick changes to a model setup without the use of a pre-processor.
Mechanical Joints in LS-Dyna for Explicit AnalysisAkshay Mistri
This document discusses different types of mechanical joints that can be modeled in LS-Dyna explicit analysis, including spherical, revolute, planar, and gear joints. It provides introductions and definitions for each joint type, along with examples of their motions and how they are defined using LS-Dyna keywords. Videos are included showing examples of each joint type in action under simulated loading conditions.
Automate your repetitive steps in Hypermesh with your own custom designed, easy to use process templates!
Reduce chances of error and provide ease of use.
The document summarizes a head performance calibration test conducted on two HIII headforms according to NHTSA test protocols. The test involved dropping the headforms to test their performance and calibration. The results showed that headform 1 passed with peak accelerations between 225-275g while headform 2 failed with peak accelerations exceeding 275g.
Effects of Occupant Protection Design Parameters in Sled TestingAkshay Mistri
This summarizes the various parameters involved for Occupant Protection such as airbag pressure and volume, seat-belt sensor timings and importance of knee air-bags.
Structural Analysis of Toyota RAV4 and its Convertible versionAkshay Mistri
Structural Analysis of Toyota RAV4 using test protocols of National Highway and Traffic Safety Administration (NHTSA) and Insurance Institute for Highway Safety (IIHS) .
Setting up a crash simulation in LS-DynaAkshay Mistri
This document provides steps to set up a crash simulation in LS-Dyna of an aluminum rail crashing into a rigid wall. It describes importing the rail model, defining the wall, applying mass to one end of the rail, assigning material properties of aluminum to the rail, applying an initial velocity to the rail, setting the simulation time and output steps, defining a special node for high resolution output, and configuring the simulation to output force on the wall, material data and displacement of the special node. Running the simulation would show the crash results and special outputs in the LS-Dyna software.
Buckling Frequencies for Beams in HypermeshAkshay Mistri
This document provides steps to model a hypermesh frame in Hyperworks to analyze buckling frequencies. It describes defining beam cross sections, materials, properties, nodes, beams, constraints, loads, buckling load collectors, loadsteps, and performing an analysis to obtain the first two buckling frequencies. Key steps include creating a steel material, rectangular beam section, applying pinned constraints to nodes C and A, a 1N load on node B, and using buckling load collectors and loadsteps to output the buckling frequencies in Hyperview.
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The document lists the natural frequencies and mode shapes obtained from a program that analyzed 10 blocks. The natural frequencies are given for each of the 10 blocks, ranging from 0.1230 to 0.8553. The mode shapes are provided as 10 vectors that describe the behavior of each block at the different natural frequencies.
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Report on Planar Vehicle Dynamics. Model included observing dynamic states of vehicle using linear and non linear tire models with 3 degrees of freedom.
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2. The first modeling elements created are nodes, which are points defined by X, Y, Z coordinates. Lines are then formed by connecting two nodes.
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Online train ticket booking system project.pdfKamal Acharya
Rail transport is one of the important modes of transport in India. Now a days we
see that there are railways that are present for the long as well as short distance
travelling which makes the life of the people easier. When compared to other
means of transport, a railway is the cheapest means of transport. The maintenance
of the railway database also plays a major role in the smooth running of this
system. The Online Train Ticket Management System will help in reserving the
tickets of the railways to travel from a particular source to the destination.
This is an overview of my career in Aircraft Design and Structures, which I am still trying to post on LinkedIn. Includes my BAE Systems Structural Test roles/ my BAE Systems key design roles and my current work on academic projects.
Sachpazis_Consolidation Settlement Calculation Program-The Python Code and th...Dr.Costas Sachpazis
Consolidation Settlement Calculation Program-The Python Code
By Professor Dr. Costas Sachpazis, Civil Engineer & Geologist
This program calculates the consolidation settlement for a foundation based on soil layer properties and foundation data. It allows users to input multiple soil layers and foundation characteristics to determine the total settlement.
2. What are theories of failure?
• Material strengths are determined from uni-axial tension tests.
• Thus, the strengths obtained from those tension tests cannot be directly used for component design since, in
actual scenarios components undergo multi-axial stress conditions.
• Hence, to use the strengths determined from tension tests to design mechanical components under any
condition of static loading, theories of failure are used.
3. How many theories are there?
• Maximum Principal Stress Theory (Rankine’s Theory).
• Maximum Shear Stress Theory (Tresca-Guest Theory).
• Maximum Principal Strain Theory (Venant’s Theory).
• Total Strain Energy Theory (Haigh’s Theory).
• Maximum Distortion Energy Theory (Von-Mises and Hencky’s Theory).
4. Maximum Principal Stress Theory
• Designed for brittle materials.
• Can be used for ductile materials in special occasions:
• Uni-axial or bi-axial loading (if principal stresses are of similar nature).
• Hydrostatic stress condition (no shear stresses).
• Condition for safe design:
→ Maximum principal stress (𝜎1) ≤ Permissible stress (𝜎 𝑝𝑒𝑟, shown below).
→ 𝜎1 ≤
𝑆 𝑦𝑡
𝑁 or 𝑆 𝑢𝑡
𝑁
Where:
• 𝑆 𝑦𝑡 and 𝑆 𝑢𝑡 are yield strength and ultimate strength, respectively.
• N is the factor of safety.
6. Maximum Shear Stress Theory
• Suitable for ductile materials as these are weak in shear.
• Gives over safe design which could be uneconomic sometimes.
• Condition for safe design:
→ Max. shear stress ( 𝜏 𝑚𝑎𝑥) ≤ Permissible shear stress ( 𝜏 𝑝𝑒𝑟).
→ 𝜏 𝑚𝑎𝑥 ≤
𝑆 𝑦𝑡
2𝑁.
→ For 3D stresses, larger of {|𝜎1 - 𝜎2|, |𝜎2 - 𝜎3|, |𝜎3 - 𝜎1|} ≤
𝑆 𝑦𝑡
𝑁.
→ For biaxial state, 𝜎3 = 0, |𝜎1| ≤
𝑆 𝑦𝑡
𝑁 when 𝜎1, 𝜎2 are like in nature, else,
|𝜎1 − 𝜎2| ≤
𝑆 𝑦𝑡
𝑁.
8. Maximum Principal Strain Theory
• Condition for safe design,
→ Max. Principal Strain (∈1) ≤ Permissible Strain (∈ 𝑌.𝑃
𝑁). Where ∈ 𝑌.𝑃 is strain at yield.
→ ∈1 ≤ 𝑆 𝑌.𝑇
𝐸𝑁. Where 𝑆 𝑌.𝑇 is yield strength,
→
1
𝐸
[𝜎1 - µ(𝜎2 + 𝜎3 )] ≤ 𝑆 𝑌.𝑇
𝐸𝑁 . E is Youngs modulus,
→ 𝜎1 - µ(𝜎2 + 𝜎3 ) ≤ 𝑆 𝑌.𝑇
𝑁 . N is factor of safety.
9. • Safe zone : Area inside the rhombus
• For biaxial state of stress , condition for safe design,
• 𝜎1 - µ(𝜎2)] ≤ 𝑆 𝑌.𝑇
𝑁
Maximum Principal Strain Theory
10. Total Strain Energy Theory
• Condition for safe design,
→ Total Strain Energy per unit volume (TSE/vol) ≤ Strain energy per unit volume at yield point.
→ 1
2 [𝜎1 ∈1+ 𝜎2 ∈2+ 𝜎3 ∈3] ≤ 1
2 𝜎 𝐸.𝐿 ∈ 𝐸.𝐿. - (1) Where E.L elastic limit,
∈1 = 1
𝐸[𝜎1 - µ(𝜎2 + 𝜎3)] ; similarly ∈2 and ∈3 . - (a), (b), (c)
→ Using (a), (b), (c) in (1), we get
→ [LHS] = TSE/vol = 1
2𝐸 [𝜎1
2
+ 𝜎2
2
+ 𝜎3
2
-2 µ(𝜎1 𝜎2+ 𝜎2 𝜎3 + 𝜎3 𝜎1) ] - (2)
→ [RHS] = For [TSE/vol] at yield point we can use, 𝜎1 = 𝜎 = 𝑆 𝑌.𝑇
𝑁 , 𝜎2 = 𝜎3 = 0. in (2),
to get TSE/vol at yield = 1
2𝐸 (
𝑆 𝑦𝑡
𝑁)2
• Therefore, condition for safe design : 𝜎1
2
+ 𝜎2
2
+ 𝜎3
2
-2 µ(𝜎1 𝜎2+ 𝜎2 𝜎3 + 𝜎3 𝜎1) ≤ (
𝑆 𝑦𝑡
𝑁)2
11. • Safe zone : Area inside the ellipse
• For biaxial state of stress ( 𝜎3= 0), condition for safe design,
• 𝜎1
2
+ 𝜎2
2
-2 µ𝜎1 𝜎2 ≤ (
𝑆 𝑦𝑡
𝑁)2
Total Strain Energy Theory
12. Total Distortion Energy Theory
• Condition for safe design,
→ Max Distortion Energy per unit volume (DE/vol) ≤ Distortion energy per unit volume at yield point (DE/Vol @ yield).
→ Now, TSE/vol = Volumetric SE/Vol + DE/Vol
→ DE/Vol = TSE/vol - Volumetric SE/Vol ; Here we already know TSE/Vol from equation 2 in slide 7.
→ Volumetric SE/Vol = ½ (Avg. Stress)(Volumetric Strain)
= 1
2 ( 𝜎1+ 𝜎2+ 𝜎3
3 )[(1 −2µ
𝐸 ) (𝜎1 + 𝜎2 + 𝜎3 )]
→ Substituting the above we get, DE/Vol = 1+ µ
6𝐸 [(𝜎1− 𝜎2)2
+ (𝜎2− 𝜎3)2
+ (𝜎3− 𝜎1)2
] - (1)
At yield point 𝜎1 = 𝜎 = 𝑆 𝑌.𝑇
𝑁 , 𝜎2 = 𝜎3 = 0 - (2)
→ Using (2) in (1), DE/Vol @ yield = 1+ µ
3𝐸 ( 𝑆 𝑌.𝑇
𝑁 )
2
• Therefore, condition for safe design: [(𝜎1− 𝜎2)2
+ (𝜎2− 𝜎3)2
+ (𝜎3− 𝜎1)2
] ≤ 2 ( 𝑆 𝑌.𝑇
𝑁 )
2
13. • Safe zone : Area inside the ellipse
• For biaxial state of stress ( 𝜎3= 0), condition for safe design,
• 𝜎1
2
+ 𝜎2
2
- 𝜎1 𝜎2 ≤ ( 𝑆 𝑌.𝑇
𝑁 )
2
Total Distortion Energy Theory
14. References
• The Gate Academy: http://thegateacademy.com/files/wppdf/Theories-of-failure.pdf
• Book: Introduction to Machine Design by VB Bhandari
• NPTEL: https://nptel.ac.in/course.html