The document discusses the concepts of centroid and centre of gravity. It defines centroid as the point where the whole area of a plane figure can be assumed to be concentrated. The centre of gravity is the point where the entire weight of a body acts and can be balanced. The document then provides methods to determine the centroid of common geometric shapes such as rectangles, triangles, semicircles, and composite shapes using the principle of moments. It includes examples of calculating the x- and y-coordinates of the centroid for various geometric problems.
This document discusses the concept of centroid and provides formulas to calculate the centroid of different geometric shapes. It defines centroid as the point within an object where the downward force of gravity appears to act. The centroid allows an object to remain balanced when placed on a pivot at the centroid point. Formulas are given for finding the centroid of triangles, rectangles, circles, semicircles, right circular cones, and composite figures. Real-life applications of centroid calculation in construction and engineering are also mentioned.
1. The document discusses stresses in solids due to eccentric and combined loading, including bending and direct stresses.
2. It defines the core of a section as the area where a load can be applied without causing tensile stress. For a rectangular section, the core is a rhombus with diagonals of B/3 and D/3.
3. Wind loading on structures like walls and chimneys is also analyzed, calculating bending moments and resultant stresses. Maintaining compressive stresses only is important for structural integrity.
The document discusses the differences between centroid and center of gravity. The centroid is defined as a point about which the entire line, area or volume is assumed to be concentrated, and is related to the distribution of length, area and volume. The center of gravity is defined as the point about which the entire weight of an object is assumed to be concentrated, also known as the center of mass, and is related to the distribution of mass. Examples are provided to illustrate the concepts of centroid and center of gravity.
This document provides information about moment of inertia including:
- Definitions of terms like center of gravity, radius of gyration, section modulus, and moment of inertia.
- Formulas for calculating moment of inertia of basic geometric sections and symmetrical/unsymmetrical sections about various axes.
- Examples of finding the center of gravity and moment of inertia of different cross-sections like rectangles, circles, T-sections, and L-sections.
this is a ppt on centroid,covering centroid of regular figures and there is a example of a composite figure,it has applications,uses of centroid,it is use ful for engineering students,it has 15 slides.
by -nishant kumar.
nk18052001@gmail.com
The document discusses the concept of the center of gravity or centroid of a body. It defines the center of gravity as the point where the entire weight of a body can be considered to be concentrated. The center of gravity is determined by the distribution of mass in the body. The document outlines different methods for calculating the centroid based on whether the body can be modeled as a line, area, or volume. It also notes that if a body has an axis of symmetry, its centroid must lie along that axis, or at the intersection of axes if it has multiple symmetries.
The document defines several terms:
1. Centroid - The point at which the total area of a plane is concentrated. It is where the average position of the total weight of the plane would balance.
2. Radius of gyration - The distance from the axis of rotation to the centroid. It is calculated as the square root of the moment of inertia divided by the total area.
3. Area moment of inertia - The product of the plane area and the square of the perpendicular distance to the axis of reference. It is a measure of the resistance offered by a plane figure to bending or twisting about an axis.
This document discusses the shear center of beam sections. It defines the shear center as the point where a load can be applied to cause pure bending without any twisting. It then provides properties of the shear center, including that it lies on the axis of symmetry for some sections. Methods for determining the location of the shear center are presented, including using the first moment of area. Real-life examples of applying shear center concepts to purlins and channel sections are given. The document concludes with an example problem of locating the shear center and calculating shear stresses for a hat section.
This document discusses the concept of centroid and provides formulas to calculate the centroid of different geometric shapes. It defines centroid as the point within an object where the downward force of gravity appears to act. The centroid allows an object to remain balanced when placed on a pivot at the centroid point. Formulas are given for finding the centroid of triangles, rectangles, circles, semicircles, right circular cones, and composite figures. Real-life applications of centroid calculation in construction and engineering are also mentioned.
1. The document discusses stresses in solids due to eccentric and combined loading, including bending and direct stresses.
2. It defines the core of a section as the area where a load can be applied without causing tensile stress. For a rectangular section, the core is a rhombus with diagonals of B/3 and D/3.
3. Wind loading on structures like walls and chimneys is also analyzed, calculating bending moments and resultant stresses. Maintaining compressive stresses only is important for structural integrity.
The document discusses the differences between centroid and center of gravity. The centroid is defined as a point about which the entire line, area or volume is assumed to be concentrated, and is related to the distribution of length, area and volume. The center of gravity is defined as the point about which the entire weight of an object is assumed to be concentrated, also known as the center of mass, and is related to the distribution of mass. Examples are provided to illustrate the concepts of centroid and center of gravity.
This document provides information about moment of inertia including:
- Definitions of terms like center of gravity, radius of gyration, section modulus, and moment of inertia.
- Formulas for calculating moment of inertia of basic geometric sections and symmetrical/unsymmetrical sections about various axes.
- Examples of finding the center of gravity and moment of inertia of different cross-sections like rectangles, circles, T-sections, and L-sections.
this is a ppt on centroid,covering centroid of regular figures and there is a example of a composite figure,it has applications,uses of centroid,it is use ful for engineering students,it has 15 slides.
by -nishant kumar.
nk18052001@gmail.com
The document discusses the concept of the center of gravity or centroid of a body. It defines the center of gravity as the point where the entire weight of a body can be considered to be concentrated. The center of gravity is determined by the distribution of mass in the body. The document outlines different methods for calculating the centroid based on whether the body can be modeled as a line, area, or volume. It also notes that if a body has an axis of symmetry, its centroid must lie along that axis, or at the intersection of axes if it has multiple symmetries.
The document defines several terms:
1. Centroid - The point at which the total area of a plane is concentrated. It is where the average position of the total weight of the plane would balance.
2. Radius of gyration - The distance from the axis of rotation to the centroid. It is calculated as the square root of the moment of inertia divided by the total area.
3. Area moment of inertia - The product of the plane area and the square of the perpendicular distance to the axis of reference. It is a measure of the resistance offered by a plane figure to bending or twisting about an axis.
This document discusses the shear center of beam sections. It defines the shear center as the point where a load can be applied to cause pure bending without any twisting. It then provides properties of the shear center, including that it lies on the axis of symmetry for some sections. Methods for determining the location of the shear center are presented, including using the first moment of area. Real-life examples of applying shear center concepts to purlins and channel sections are given. The document concludes with an example problem of locating the shear center and calculating shear stresses for a hat section.
Bending Stresses are important in the design of beams from strength point of view. The present source gives an idea on theory and problems in bending stresses.
Unit 5 - deflection of beams and columnskarthi keyan
1) The document discusses various methods for calculating beam deflections, including double integration, Macaulay's method, and moment area methods.
2) It also covers columns, struts, and the different types of column structures. The slenderness ratio and effective length are important parameters for columns.
3) Short columns fail due to crushing while long columns fail due to bending or buckling. The crippling or buckling load is also discussed.
The document discusses compound stresses, which involve both normal and shear stresses acting on a plane. It provides equations to calculate:
1) Normal and shear stresses on a plane inclined to the given stress plane.
2) The inclination and normal stresses on the planes of maximum and minimum normal stress (principal planes).
3) The inclination and shear stresses on the planes of maximum shear stress.
It includes an example problem calculating the principal stresses and maximum shear stresses given a state of stress. Sign conventions for stresses are also defined.
The document discusses beams, which are horizontal structural members that support applied loads. It defines applied and reactive forces, and describes different types of supports including roller, hinge, and fixed supports. It then defines and describes different types of beams, including cantilever, simply supported, overhanging, fixed, and continuous beams. It also discusses types of loads, including concentrated and distributed loads, and how beams experience both bending and shear forces from loads.
This document compares the Bernoulli-Euler beam theory and Timoshenko beam theory. [1] The Timoshenko beam theory accounts for transverse shear deformation, which the classical Bernoulli-Euler theory neglects. [2] The finite element models of the two theories are derived, with the Timoshenko model having a larger stiffness matrix that accounts for the additional degree of freedom from shear deformation. [3] An example problem of a simply supported beam is solved analytically and using finite elements to demonstrate the difference between the two theories.
Ekeeda Provides Online Video Lectures for Civil Engineering Degree Subject Courses for All Engineering Universities. Visit us: https://ekeeda.com/streamdetails/stream/civil-engineering
This document discusses beam deflection. It begins by defining beam deflection and the factors that affect it, including bending moment, material properties, and shape properties. It then presents the general formula for calculating beam deflection using double integration of the bending moment equation. Examples are given of using boundary conditions to solve for deflection in simply supported beams, cantilever beams, and beams under various loading types. Common deflection formulas are also presented.
This document discusses stresses in beams. It covers bending stresses, shear stresses, deflection in beams, and torsion in solid and hollow shafts. The key assumptions in beam bending theory are outlined. Bending stresses are explained, including the location of the neutral axis and how stresses vary through the beam cross-section based on the bending moment and geometry. Section modulus is defined as the ratio of the moment of inertia to the distance of the outermost fiber from the neutral axis. Composite beams made of different materials are also discussed.
This document provides lecture notes on trusses and truss analysis. It defines a truss as consisting of straight members connected at joints, with no member continuous through a joint. Simple trusses follow the rule that the number of members m equals 2n-3, where n is the number of joints. The document describes two common methods for truss analysis: (1) the method of joints, which uses equilibrium equations at each joint to solve for member forces, and (2) the method of sections, which uses equilibrium of a portion of the truss cut out by a section. Sample problems demonstrate applying each method to determine member forces in specific trusses.
The document discusses bending stresses in beams. It begins by outlining simplifying assumptions made in deriving the flexure formula to relate bending stresses to bending moments. These assumptions include plane sections remaining plane and perpendicular to the deformed beam axis. The neutral axis is defined as the axis where longitudinal fibers experience no deformation.
The derivation of the flexure formula is shown. Flexural stresses are proportional to the distance from the neutral axis and bending moment. Procedures for determining stresses at given points, as well as maximum stresses, are provided. Sample problems demonstrate applying the flexure formula and finding maximum stresses for different beam cross sections.
This document provides an introduction to using definite integrals to calculate volumes, lengths of curves, centers of mass, surface areas, work, and fluid forces. It discusses calculating volumes through slicing solids and rotating areas about an axis. Examples are provided for finding the volumes of pyramids, wedges, and solids of revolution. It also discusses using integrals to find curve lengths, circle circumferences, and moments and centers of mass for various objects. Surface areas of revolution and fluid pressures are also explained.
This document discusses bending stresses in beams. It defines simple or pure bending as when a beam experiences zero shear force and constant bending moment over a length. For simple bending, the stress distribution can be calculated using beam theory. The key points are:
- Bending stresses are introduced due to bending moments and are highest at the extreme fibers furthest from the neutral axis.
- The neutral axis experiences no bending stress and its location is defined by the centroidal axis of the beam cross-section.
- Bending stress is directly proportional to the distance from the neutral axis. The stress distribution follows σ = My/I, where M is the bending moment, y is the distance from neutral axis, and I is
The document discusses bending stresses in beams. It describes how bending stresses are developed in beams to resist bending moments and shearing forces. The theory of pure bending is introduced, where only bending stresses are considered without the effect of shear. Equations for calculating bending stresses are derived based on the beam's moment of inertia, bending moment, and distance from the neutral axis. Several beam cross-section examples are provided to demonstrate how to calculate the maximum bending stress and section modulus.
This document discusses stresses in beams and beam deflection. It covers several methods for analyzing bending stresses and deflection in beams, including: [1] the engineering beam theory relating moment, curvature, and stress; [2] double integration and moment area methods for calculating slope and deflection; and [3] Macaulay's method, which simplifies calculations for beams with eccentric loads. Formulas are provided relating bending moment, shear force, curvature, slope, and deflection. Moment-area theorems are also described for relating bending moment to slope and deflection.
Lecture 9 shear force and bending moment in beamsDeepak Agarwal
The document discusses stresses in beams. It covers topics like shear force and bending moment diagrams, bending stresses, shear stresses, deflection, and torsion. Beams are structural members subjected to transverse forces that induce bending. Stresses and strains are created within beams when loaded. Shear forces and bending moments allow determining these internal stresses and maintaining equilibrium. Formulas are provided for calculating shear forces and bending moments in different beam configurations like cantilevers, simply supported beams, and beams with various load types.
This document provides information about shear stresses and shear force in structures. It includes:
- Definitions of shear force and shear stress. Shear force is an unbalanced force parallel to a cross-section, and shear stress develops to resist the shear force.
- Explanations of horizontal and vertical shear stresses that develop in beams due to bending moments. Shear stress is highest at the neutral axis and reduces towards the top and bottom of the beam cross-section.
- Derivations of formulas for calculating shear stress across different beam cross-sections. Shear stress is directly proportional to the shear force and beam geometry.
- Examples of calculating maximum and average shear stresses for various cross-sections
- The normal stress distribution in a curved beam is hyperbolic and determined using specialized formulas, as the neutral axis does not pass through the centroid due to curvature.
- To analyze a curved beam, one must first determine the cross-sectional properties and location of the neutral axis, then calculate the normal stress distribution using the appropriate formula.
- For a rectangular steel bar bent into a circular arc, the maximum moment that can be applied before exceeding the allowable stress is 0.174 kN-m, with maximum stress at the bottom of the bar. If the bar was straight, the maximum moment would be 0.187 kN-m.
1. The document discusses principal stresses and planes, describing how to determine the maximum and minimum normal stresses (principal stresses) and their corresponding planes from a state of plane stress.
2. It introduces Mohr's circle as a graphical method to determine principal stresses and maximum shear stresses from the stresses on any plane.
3. Equations are derived relating the principal stresses and maximum shear stress to the normal and shear stresses on any plane using trigonometric functions of the angle between the plane and principal planes.
This document discusses unsymmetrical bending of beams. Unsymmetrical bending occurs when the beam cross-section is not symmetrical about the plane of bending, or when the load line does not pass through a principal axis of the cross-section. The document defines principal axes as those passing through the centroid where the product of inertia is zero. It presents equations to calculate the principal moments of inertia and product of inertia for a given cross-section, and describes how to determine the principal axes by setting the product of inertia equal to zero.
Chapter 7: Shear Stresses in Beams and Related ProblemsMonark Sutariya
This document discusses shear stresses in beams. It defines shear stress and shear flow, and describes how to calculate them using the shear stress formula. It discusses limitations of this formula and how shear stresses behave in beam flanges and at boundaries. The concept of the shear center is introduced as the point where an applied force will not cause twisting. Methods for combining direct and torsional shear stresses are also covered.
This document discusses calculating the moment of inertia for composite cross-sections made up of multiple simple geometric shapes. It introduces the parallel axis theorem, which allows calculating the moment of inertia of each individual shape about a common reference axis so that the individual values can be added to determine the total moment of inertia of the composite cross-section. Several examples are provided to demonstrate calculating moments of inertia for composite areas using this approach.
Bending Stresses are important in the design of beams from strength point of view. The present source gives an idea on theory and problems in bending stresses.
Unit 5 - deflection of beams and columnskarthi keyan
1) The document discusses various methods for calculating beam deflections, including double integration, Macaulay's method, and moment area methods.
2) It also covers columns, struts, and the different types of column structures. The slenderness ratio and effective length are important parameters for columns.
3) Short columns fail due to crushing while long columns fail due to bending or buckling. The crippling or buckling load is also discussed.
The document discusses compound stresses, which involve both normal and shear stresses acting on a plane. It provides equations to calculate:
1) Normal and shear stresses on a plane inclined to the given stress plane.
2) The inclination and normal stresses on the planes of maximum and minimum normal stress (principal planes).
3) The inclination and shear stresses on the planes of maximum shear stress.
It includes an example problem calculating the principal stresses and maximum shear stresses given a state of stress. Sign conventions for stresses are also defined.
The document discusses beams, which are horizontal structural members that support applied loads. It defines applied and reactive forces, and describes different types of supports including roller, hinge, and fixed supports. It then defines and describes different types of beams, including cantilever, simply supported, overhanging, fixed, and continuous beams. It also discusses types of loads, including concentrated and distributed loads, and how beams experience both bending and shear forces from loads.
This document compares the Bernoulli-Euler beam theory and Timoshenko beam theory. [1] The Timoshenko beam theory accounts for transverse shear deformation, which the classical Bernoulli-Euler theory neglects. [2] The finite element models of the two theories are derived, with the Timoshenko model having a larger stiffness matrix that accounts for the additional degree of freedom from shear deformation. [3] An example problem of a simply supported beam is solved analytically and using finite elements to demonstrate the difference between the two theories.
Ekeeda Provides Online Video Lectures for Civil Engineering Degree Subject Courses for All Engineering Universities. Visit us: https://ekeeda.com/streamdetails/stream/civil-engineering
This document discusses beam deflection. It begins by defining beam deflection and the factors that affect it, including bending moment, material properties, and shape properties. It then presents the general formula for calculating beam deflection using double integration of the bending moment equation. Examples are given of using boundary conditions to solve for deflection in simply supported beams, cantilever beams, and beams under various loading types. Common deflection formulas are also presented.
This document discusses stresses in beams. It covers bending stresses, shear stresses, deflection in beams, and torsion in solid and hollow shafts. The key assumptions in beam bending theory are outlined. Bending stresses are explained, including the location of the neutral axis and how stresses vary through the beam cross-section based on the bending moment and geometry. Section modulus is defined as the ratio of the moment of inertia to the distance of the outermost fiber from the neutral axis. Composite beams made of different materials are also discussed.
This document provides lecture notes on trusses and truss analysis. It defines a truss as consisting of straight members connected at joints, with no member continuous through a joint. Simple trusses follow the rule that the number of members m equals 2n-3, where n is the number of joints. The document describes two common methods for truss analysis: (1) the method of joints, which uses equilibrium equations at each joint to solve for member forces, and (2) the method of sections, which uses equilibrium of a portion of the truss cut out by a section. Sample problems demonstrate applying each method to determine member forces in specific trusses.
The document discusses bending stresses in beams. It begins by outlining simplifying assumptions made in deriving the flexure formula to relate bending stresses to bending moments. These assumptions include plane sections remaining plane and perpendicular to the deformed beam axis. The neutral axis is defined as the axis where longitudinal fibers experience no deformation.
The derivation of the flexure formula is shown. Flexural stresses are proportional to the distance from the neutral axis and bending moment. Procedures for determining stresses at given points, as well as maximum stresses, are provided. Sample problems demonstrate applying the flexure formula and finding maximum stresses for different beam cross sections.
This document provides an introduction to using definite integrals to calculate volumes, lengths of curves, centers of mass, surface areas, work, and fluid forces. It discusses calculating volumes through slicing solids and rotating areas about an axis. Examples are provided for finding the volumes of pyramids, wedges, and solids of revolution. It also discusses using integrals to find curve lengths, circle circumferences, and moments and centers of mass for various objects. Surface areas of revolution and fluid pressures are also explained.
This document discusses bending stresses in beams. It defines simple or pure bending as when a beam experiences zero shear force and constant bending moment over a length. For simple bending, the stress distribution can be calculated using beam theory. The key points are:
- Bending stresses are introduced due to bending moments and are highest at the extreme fibers furthest from the neutral axis.
- The neutral axis experiences no bending stress and its location is defined by the centroidal axis of the beam cross-section.
- Bending stress is directly proportional to the distance from the neutral axis. The stress distribution follows σ = My/I, where M is the bending moment, y is the distance from neutral axis, and I is
The document discusses bending stresses in beams. It describes how bending stresses are developed in beams to resist bending moments and shearing forces. The theory of pure bending is introduced, where only bending stresses are considered without the effect of shear. Equations for calculating bending stresses are derived based on the beam's moment of inertia, bending moment, and distance from the neutral axis. Several beam cross-section examples are provided to demonstrate how to calculate the maximum bending stress and section modulus.
This document discusses stresses in beams and beam deflection. It covers several methods for analyzing bending stresses and deflection in beams, including: [1] the engineering beam theory relating moment, curvature, and stress; [2] double integration and moment area methods for calculating slope and deflection; and [3] Macaulay's method, which simplifies calculations for beams with eccentric loads. Formulas are provided relating bending moment, shear force, curvature, slope, and deflection. Moment-area theorems are also described for relating bending moment to slope and deflection.
Lecture 9 shear force and bending moment in beamsDeepak Agarwal
The document discusses stresses in beams. It covers topics like shear force and bending moment diagrams, bending stresses, shear stresses, deflection, and torsion. Beams are structural members subjected to transverse forces that induce bending. Stresses and strains are created within beams when loaded. Shear forces and bending moments allow determining these internal stresses and maintaining equilibrium. Formulas are provided for calculating shear forces and bending moments in different beam configurations like cantilevers, simply supported beams, and beams with various load types.
This document provides information about shear stresses and shear force in structures. It includes:
- Definitions of shear force and shear stress. Shear force is an unbalanced force parallel to a cross-section, and shear stress develops to resist the shear force.
- Explanations of horizontal and vertical shear stresses that develop in beams due to bending moments. Shear stress is highest at the neutral axis and reduces towards the top and bottom of the beam cross-section.
- Derivations of formulas for calculating shear stress across different beam cross-sections. Shear stress is directly proportional to the shear force and beam geometry.
- Examples of calculating maximum and average shear stresses for various cross-sections
- The normal stress distribution in a curved beam is hyperbolic and determined using specialized formulas, as the neutral axis does not pass through the centroid due to curvature.
- To analyze a curved beam, one must first determine the cross-sectional properties and location of the neutral axis, then calculate the normal stress distribution using the appropriate formula.
- For a rectangular steel bar bent into a circular arc, the maximum moment that can be applied before exceeding the allowable stress is 0.174 kN-m, with maximum stress at the bottom of the bar. If the bar was straight, the maximum moment would be 0.187 kN-m.
1. The document discusses principal stresses and planes, describing how to determine the maximum and minimum normal stresses (principal stresses) and their corresponding planes from a state of plane stress.
2. It introduces Mohr's circle as a graphical method to determine principal stresses and maximum shear stresses from the stresses on any plane.
3. Equations are derived relating the principal stresses and maximum shear stress to the normal and shear stresses on any plane using trigonometric functions of the angle between the plane and principal planes.
This document discusses unsymmetrical bending of beams. Unsymmetrical bending occurs when the beam cross-section is not symmetrical about the plane of bending, or when the load line does not pass through a principal axis of the cross-section. The document defines principal axes as those passing through the centroid where the product of inertia is zero. It presents equations to calculate the principal moments of inertia and product of inertia for a given cross-section, and describes how to determine the principal axes by setting the product of inertia equal to zero.
Chapter 7: Shear Stresses in Beams and Related ProblemsMonark Sutariya
This document discusses shear stresses in beams. It defines shear stress and shear flow, and describes how to calculate them using the shear stress formula. It discusses limitations of this formula and how shear stresses behave in beam flanges and at boundaries. The concept of the shear center is introduced as the point where an applied force will not cause twisting. Methods for combining direct and torsional shear stresses are also covered.
This document discusses calculating the moment of inertia for composite cross-sections made up of multiple simple geometric shapes. It introduces the parallel axis theorem, which allows calculating the moment of inertia of each individual shape about a common reference axis so that the individual values can be added to determine the total moment of inertia of the composite cross-section. Several examples are provided to demonstrate calculating moments of inertia for composite areas using this approach.
This document discusses moment of inertia, which is a measure of an object's resistance to changes in rotation. It begins by defining moment of inertia as the second moment of force or mass of an object. It then provides formulas for calculating the moment of inertia of common shapes like rectangles, circles, and hollow sections. For rectangles, the moment of inertia depends on the cube of the distance of the axis from the object's sides. For circles, the moment of inertia is proportional to the diameter to the fourth power. The document also presents theorems for calculating moment of inertia about different axes, such as perpendicular axes and parallel axes. Sample problems are worked through to demonstrate calculating moment of inertia for rectangular and circular sections.
Centroid and Moment of Inertia from mechanics of material by hibbler related ...FREE LAUNCER
Centroids and moment of inertia are important concepts in mechanics. The centroid of a plane figure is the point where the entire area is considered to be concentrated. It is found by suspending the figure from different corners and finding the intersection point of vertical lines. The center of gravity is where the entire mass is considered concentrated. For uniform plane figures with no weight, the centroid and center of gravity coincide. The moment of inertia is a measure of an object's resistance to changes in rotation or bending and depends on the object's mass distribution and axis of rotation. It is calculated based on the object's area or mass distances from the axis of rotation.
The first moment of area of a lamina is defined as the product of the lamina's area and the perpendicular distance of its center of gravity from a given axis. It is used to determine the center of gravity of an area. To calculate the first moment of area, the area is split into segments, and the area of each segment is multiplied by its distance from the axis and summed. This gives the first moment of area, which provides information about the distribution of the area.
This document discusses circles, arcs, sectors, and how to calculate their properties. It defines a circle as all points equidistant from a center point, and an arc as a portion of a circle's circumference. The length of an arc is calculated by taking the ratio of the arc's central angle measure to 360 degrees and multiplying by 2πr. Similarly, the area of a sector is calculated by taking the ratio of its central angle measure to 360 degrees and multiplying by πr^2. Several examples are provided to demonstrate calculating arc lengths and sector areas.
This document provides an overview of topics in vector integration, including line integrals, surface integrals, and volume integrals. It includes examples of calculating each type of integral. The key theorems covered are Green's theorem, Stokes' theorem, and Gauss's theorem of divergence. Green's theorem relates a line integral around a closed curve to a double integral over the enclosed region. Stokes' theorem relates a line integral around a closed curve to a surface integral over the enclosed surface. Gauss's theorem relates the surface integral of the normal component of a vector field over a closed surface to the volume integral of the divergence of the vector field over the enclosed volume.
This document presents the analysis of non-lifting potential flow past a thin symmetric hydrofoil using a finite difference method. The objectives are to solve the potential flow problem around a 2D hydrofoil and calculate the pressure distribution. A NACA 0012 hydrofoil is used. Governing equations and boundary conditions for the potential flow are described. A structured algebraic grid is used to generate points around the hydrofoil. Finite difference equations are derived and discretized on the grid points. The pressure coefficient is then calculated and compared to experimental results, showing good agreement.
Prof. V. V. Nalawade, Notes CGMI with practice numericalVrushali Nalawade
Centre of gravity is a point where the whole weight of the body is assumed to act. i.e., it is a point where entire distribution of gravitational force is supposed to be concentrated
It is generally denoted “G” for all three dimensional rigid bodies.
e.g. Sphere, table , vehicle, dam, human etc
Centroid is a point where the whole area of a plane lamina is assumed to act.
It is a point where the entire length, area & volume is supposed to be concentrated.
It is a geometrical centre of a figure.
It is used for two dimensional figures.
e.g. rectangle, circle, triangle, semicircle
Centroid is a point where the whole area of a plane lamina is assumed to act.
It is a point where the entire length, area & volume is supposed to be concentrated.
It is a geometrical centre of a figure.
It is used for two dimensional figures.
e.g. rectangle, circle, triangle, semicircle
Centroid is a point where the whole area of a plane lamina is assumed to act.
It is a point where the entire length, area & volume is supposed to be concentrated.
It is a geometrical centre of a figure.
It is used for two dimensional figures.
e.g. rectangle, circle, triangle, semicircle
The document discusses applications of integration, including calculating the length of a curve and surface area of solids obtained by rotating curves. It provides formulas for finding the arc length of a curve given by y=f(x), and surface area of solids obtained by rotating curves about the x- or y-axes. Examples are worked out applying these formulas to find the arc length of curves and surface area of rotated regions. The document also discusses evaluating triple integrals to find the volume of a three-dimensional region and using triple integrals to find the centroid of a volume.
The document discusses applications of definite integrals, including calculating the areas of planar regions and volumes of solids of revolution. It provides examples of using integrals to find the areas of regions bounded by curves and the x-axis, as well as the volumes of solids generated by rotating regions about an axis. The disc method for finding volumes of revolution is also introduced.
Properties of surfaces-Centre of gravity and Moment of InertiaJISHNU V
The document discusses properties of surfaces, including centre of gravity and moment of inertia. It defines key terms like centre of gravity, centroid, area moment of inertia, radius of gyration, and mass moment of inertia. Methods for calculating these properties are presented for basic shapes like rectangles, triangles, circles, and composite shapes. Theorems like the perpendicular axis theorem and parallel axis theorem are also covered. Examples are provided for determining the moment of inertia of various plane figures and structures.
Prof. V. V. Nalawade, UNIT-3 Centroid, Centre off Gravity and Moment of InertiaVrushali Nalawade
The document discusses concepts related to center of gravity and moment of inertia. It defines center of gravity as the point where the entire weight of a body acts and centroid as the point where the entire area of a plane figure acts. It provides formulas for calculating the centroid of composite figures and discusses the parallel axis theorem and perpendicular axis theorem for calculating moment of inertia about different axes. The document also defines radius of gyration and provides formulas for calculating moment of inertia and radius of gyration of common plane figures.
The document discusses rotation matrix (DCM) and quaternions. It provides the definitions and equations for representing 3D rotations using DCM and quaternions. It then gives an example of calculating the DCM, quaternion elements, and rotated axes given the Euler angles of 45.827° for roll, 12.346° for pitch, and -198.542° for yaw in a 1-2-3 rotation sequence (roll-pitch-yaw). It also provides the inverse calculation of determining the Euler angles given a quaternion of [-0.425 -0.0537 -0.1950.782].
Here are the steps to find the centroid of each given plane region:
1. Region bounded by y = 10x - x^2, x-axis, x = 2, x = 5:
- Set up the integral to find the area A: ∫2^5 (10x - x^2) dx
- Evaluate the integral: A = 96
- Set up the integrals to find the x- and y-moments: ∫2^5 x(10x - x^2) dx and ∫2^5 (10x - x^2)x dx
- Evaluate the integrals: Mx = 192, My = 960
- Use the formulas for centroid: C
On approximating the Riemannian 1-centerFrank Nielsen
This document discusses algorithms for finding the smallest enclosing ball that fully covers a set of points on a Riemannian manifold. It begins by reviewing Euclidean smallest enclosing ball algorithms, then extends the concept to Riemannian manifolds. Coreset approximations are discussed as well as gradient descent algorithms. The document provides background on Riemannian geometry concepts needed like geodesics, exponential maps, and curvature. Overall, it presents algorithms to generalize the smallest enclosing ball problem to points on Riemannian manifolds.
This document describes algorithms for X-ray and maximum intensity projection (MIP) volume rendering. It provides pseudocode for the X-ray and MIP rendering algorithms, which involve casting rays through a volumetric dataset and accumulating or finding the maximum intensity values along each ray. Key steps include intersecting rays with the volume bounding box, trilinear interpolation of sample values, and scaling and rotating the rendered image. Code fragments are presented that implement functions for X-ray and MIP rendering based on these algorithms.
Rotation in 3d Space: Euler Angles, Quaternions, Marix DescriptionsSolo Hermelin
Mathematics of rotation in 3d space, a lecture that I've prepared.
This presentation is at a Undergraduate in Science (Math, Physics, Engineering) level.
Please send comments and suggestions to solo.hermelin@gmail.com. Thanks!
Fore more presentations, please visit my website at
http://www.solohermelin.com/
Null Bangalore | Pentesters Approach to AWS IAMDivyanshu
#Abstract:
- Learn more about the real-world methods for auditing AWS IAM (Identity and Access Management) as a pentester. So let us proceed with a brief discussion of IAM as well as some typical misconfigurations and their potential exploits in order to reinforce the understanding of IAM security best practices.
- Gain actionable insights into AWS IAM policies and roles, using hands on approach.
#Prerequisites:
- Basic understanding of AWS services and architecture
- Familiarity with cloud security concepts
- Experience using the AWS Management Console or AWS CLI.
- For hands on lab create account on [killercoda.com](https://killercoda.com/cloudsecurity-scenario/)
# Scenario Covered:
- Basics of IAM in AWS
- Implementing IAM Policies with Least Privilege to Manage S3 Bucket
- Objective: Create an S3 bucket with least privilege IAM policy and validate access.
- Steps:
- Create S3 bucket.
- Attach least privilege policy to IAM user.
- Validate access.
- Exploiting IAM PassRole Misconfiguration
-Allows a user to pass a specific IAM role to an AWS service (ec2), typically used for service access delegation. Then exploit PassRole Misconfiguration granting unauthorized access to sensitive resources.
- Objective: Demonstrate how a PassRole misconfiguration can grant unauthorized access.
- Steps:
- Allow user to pass IAM role to EC2.
- Exploit misconfiguration for unauthorized access.
- Access sensitive resources.
- Exploiting IAM AssumeRole Misconfiguration with Overly Permissive Role
- An overly permissive IAM role configuration can lead to privilege escalation by creating a role with administrative privileges and allow a user to assume this role.
- Objective: Show how overly permissive IAM roles can lead to privilege escalation.
- Steps:
- Create role with administrative privileges.
- Allow user to assume the role.
- Perform administrative actions.
- Differentiation between PassRole vs AssumeRole
Try at [killercoda.com](https://killercoda.com/cloudsecurity-scenario/)
Embedded machine learning-based road conditions and driving behavior monitoringIJECEIAES
Car accident rates have increased in recent years, resulting in losses in human lives, properties, and other financial costs. An embedded machine learning-based system is developed to address this critical issue. The system can monitor road conditions, detect driving patterns, and identify aggressive driving behaviors. The system is based on neural networks trained on a comprehensive dataset of driving events, driving styles, and road conditions. The system effectively detects potential risks and helps mitigate the frequency and impact of accidents. The primary goal is to ensure the safety of drivers and vehicles. Collecting data involved gathering information on three key road events: normal street and normal drive, speed bumps, circular yellow speed bumps, and three aggressive driving actions: sudden start, sudden stop, and sudden entry. The gathered data is processed and analyzed using a machine learning system designed for limited power and memory devices. The developed system resulted in 91.9% accuracy, 93.6% precision, and 92% recall. The achieved inference time on an Arduino Nano 33 BLE Sense with a 32-bit CPU running at 64 MHz is 34 ms and requires 2.6 kB peak RAM and 139.9 kB program flash memory, making it suitable for resource-constrained embedded systems.
Software Engineering and Project Management - Introduction, Modeling Concepts...Prakhyath Rai
Introduction, Modeling Concepts and Class Modeling: What is Object orientation? What is OO development? OO Themes; Evidence for usefulness of OO development; OO modeling history. Modeling
as Design technique: Modeling, abstraction, The Three models. Class Modeling: Object and Class Concept, Link and associations concepts, Generalization and Inheritance, A sample class model, Navigation of class models, and UML diagrams
Building the Analysis Models: Requirement Analysis, Analysis Model Approaches, Data modeling Concepts, Object Oriented Analysis, Scenario-Based Modeling, Flow-Oriented Modeling, class Based Modeling, Creating a Behavioral Model.
Design and optimization of ion propulsion dronebjmsejournal
Electric propulsion technology is widely used in many kinds of vehicles in recent years, and aircrafts are no exception. Technically, UAVs are electrically propelled but tend to produce a significant amount of noise and vibrations. Ion propulsion technology for drones is a potential solution to this problem. Ion propulsion technology is proven to be feasible in the earth’s atmosphere. The study presented in this article shows the design of EHD thrusters and power supply for ion propulsion drones along with performance optimization of high-voltage power supply for endurance in earth’s atmosphere.
Comparative analysis between traditional aquaponics and reconstructed aquapon...bijceesjournal
The aquaponic system of planting is a method that does not require soil usage. It is a method that only needs water, fish, lava rocks (a substitute for soil), and plants. Aquaponic systems are sustainable and environmentally friendly. Its use not only helps to plant in small spaces but also helps reduce artificial chemical use and minimizes excess water use, as aquaponics consumes 90% less water than soil-based gardening. The study applied a descriptive and experimental design to assess and compare conventional and reconstructed aquaponic methods for reproducing tomatoes. The researchers created an observation checklist to determine the significant factors of the study. The study aims to determine the significant difference between traditional aquaponics and reconstructed aquaponics systems propagating tomatoes in terms of height, weight, girth, and number of fruits. The reconstructed aquaponics system’s higher growth yield results in a much more nourished crop than the traditional aquaponics system. It is superior in its number of fruits, height, weight, and girth measurement. Moreover, the reconstructed aquaponics system is proven to eliminate all the hindrances present in the traditional aquaponics system, which are overcrowding of fish, algae growth, pest problems, contaminated water, and dead fish.
Electric vehicle and photovoltaic advanced roles in enhancing the financial p...IJECEIAES
Climate change's impact on the planet forced the United Nations and governments to promote green energies and electric transportation. The deployments of photovoltaic (PV) and electric vehicle (EV) systems gained stronger momentum due to their numerous advantages over fossil fuel types. The advantages go beyond sustainability to reach financial support and stability. The work in this paper introduces the hybrid system between PV and EV to support industrial and commercial plants. This paper covers the theoretical framework of the proposed hybrid system including the required equation to complete the cost analysis when PV and EV are present. In addition, the proposed design diagram which sets the priorities and requirements of the system is presented. The proposed approach allows setup to advance their power stability, especially during power outages. The presented information supports researchers and plant owners to complete the necessary analysis while promoting the deployment of clean energy. The result of a case study that represents a dairy milk farmer supports the theoretical works and highlights its advanced benefits to existing plants. The short return on investment of the proposed approach supports the paper's novelty approach for the sustainable electrical system. In addition, the proposed system allows for an isolated power setup without the need for a transmission line which enhances the safety of the electrical network
Redefining brain tumor segmentation: a cutting-edge convolutional neural netw...IJECEIAES
Medical image analysis has witnessed significant advancements with deep learning techniques. In the domain of brain tumor segmentation, the ability to
precisely delineate tumor boundaries from magnetic resonance imaging (MRI)
scans holds profound implications for diagnosis. This study presents an ensemble convolutional neural network (CNN) with transfer learning, integrating
the state-of-the-art Deeplabv3+ architecture with the ResNet18 backbone. The
model is rigorously trained and evaluated, exhibiting remarkable performance
metrics, including an impressive global accuracy of 99.286%, a high-class accuracy of 82.191%, a mean intersection over union (IoU) of 79.900%, a weighted
IoU of 98.620%, and a Boundary F1 (BF) score of 83.303%. Notably, a detailed comparative analysis with existing methods showcases the superiority of
our proposed model. These findings underscore the model’s competence in precise brain tumor localization, underscoring its potential to revolutionize medical
image analysis and enhance healthcare outcomes. This research paves the way
for future exploration and optimization of advanced CNN models in medical
imaging, emphasizing addressing false positives and resource efficiency.
Software Engineering and Project Management - Software Testing + Agile Method...Prakhyath Rai
Software Testing: A Strategic Approach to Software Testing, Strategic Issues, Test Strategies for Conventional Software, Test Strategies for Object -Oriented Software, Validation Testing, System Testing, The Art of Debugging.
Agile Methodology: Before Agile – Waterfall, Agile Development.
Applications of artificial Intelligence in Mechanical Engineering.pdfAtif Razi
Historically, mechanical engineering has relied heavily on human expertise and empirical methods to solve complex problems. With the introduction of computer-aided design (CAD) and finite element analysis (FEA), the field took its first steps towards digitization. These tools allowed engineers to simulate and analyze mechanical systems with greater accuracy and efficiency. However, the sheer volume of data generated by modern engineering systems and the increasing complexity of these systems have necessitated more advanced analytical tools, paving the way for AI.
AI offers the capability to process vast amounts of data, identify patterns, and make predictions with a level of speed and accuracy unattainable by traditional methods. This has profound implications for mechanical engineering, enabling more efficient design processes, predictive maintenance strategies, and optimized manufacturing operations. AI-driven tools can learn from historical data, adapt to new information, and continuously improve their performance, making them invaluable in tackling the multifaceted challenges of modern mechanical engineering.
2. CENTRE OF GRAVITY
It is the point where the whole weight of the body is assumed to be
concentrated. It is the point on which the body can be balanced.
It is the point through which the weight of the body is assumed to act. This
point is usually denoted by ‘C.G.’ or ‘G’.
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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3. CENTROID
Centroid is the point where the whole area of the plane figure is
assumed to be concentrated.
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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6. It is easy to find the centroid of simple shapes.
If the object has an axis of symmetry the centroid will always lie on
that axis.
If the object has two axes of symmetry, the centroid will be at the
intersection of the two axes.
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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10. CENTROID of a figure is always represented in a coordinate system as shown in figure
below. The calculation of centroid means the determination of 𝒙 and 𝒚.
y
x
𝒙
𝒚
𝑏
ℎ
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE 10
11. Determination of Centroid by the
Method of Moments
Let us consider a plane area A. The centre of gravity/ centroid of the area G
is located at a distance 𝒙 from the y-axis and at a distance 𝒚 from the x-axis
(the point through which the total weight W acts).
G𝒙
𝒚
A
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE 11
12. Assume the area A is divided into infinite small areas 𝑎1, 𝑎2,
𝑎3, 𝑎4…etc and their corresponding centroids are 𝑔1, 𝑔2, 𝑔3,
𝑔4…etc.
Let (𝑥1, 𝑦1), (𝑥2, 𝑦2), (𝑥3, 𝑦3) , (𝑥4, 𝑦4)….etc be the coordinates
of the centroids w.r.t x axis and y axis.
𝑎1
𝑎2 𝑎3
𝑎4
𝑎6
𝑎5
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE 12
13. Applying the principle of MOMENT of area,
Moment of Total area A about y axis = Area x centroidal distance
= A x 𝒙
Sum of moments of small areas about y axis
=𝑎1 𝑥1 + 𝑎2 𝑥2 + 𝑎3 𝑥3 + 𝑎4 𝑥4…. etc.
= 𝑎𝑥
Using Varignon’s theorem of moments,
A x 𝒙 = 𝑎𝑥
Therefore, 𝒙 =
𝒂𝒙
𝑨
Similarly, 𝒚 =
𝒂𝒚
𝑨
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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14. Axes of Reference
These are the axes with respect to
which the centroid of a given
figure is determined.
Centroidal Axis
The axis which passes through the
centroid of the given figure is known as
centroidal axis, such as
the axis X-X and the axis Y-Y shown in
Figure.
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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18. DERIVATION OF CENTROID OF
SOME IMPORTANT GEOMETRICAL
FIGURES
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE 18
19. RECTANGLE
Let us consider a rectangular lamina of area (b x d) as shown in
Figure.
Now consider a horizontal elementary strip of area (b x dy),
which is at a distance y from the reference axis AB.
Moment of area of elementary strip about AB
= (b x dy) . y
Sum of moments of such elementary strips about AB is
given by,
𝟎
𝒅
(b . dy) . y
= b 𝟎
𝒅
ydy
= b .
𝒚 𝟐
𝟐 𝟎
𝒅
=
𝒃𝒅 𝟐
𝟐
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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20. Moment of total area about AB = bd . 𝒚
Apply the principle of moments about AB,
bd . 𝒚 =
𝒃𝒅 𝟐
𝟐
𝒚 =
𝒅
𝟐
By considering a vertical strip, similarly, we can prove that
𝒙 =
𝒃
𝟐
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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21. TRIANGLE
Let us consider a triangular lamina of area ( 𝟏
𝟐 x b x d) as
shown in Figure.
Now consider a horizontal elementary strip of area (𝒃 𝟏 x dy),
which is at a distance y from the reference axis AB.
Using the property of similar triangles, we have
𝑏1
𝑏
=
𝑑 −𝑦
𝑑
𝑏1=
𝑑 −𝑦
𝑑
. b
Area of the elementary strip =
𝒅 −𝒚
𝒅
. b . dy
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE 21
22. Moment of area of elementary strip about AB
= Area x y
=
𝒅 −𝒚
𝒅
. b . dy. y
Sum of moments of such elementary strips is given by
=
=
𝒃𝒅 𝟐
𝟔
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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23. Whereas, 𝒙 =
𝒃
𝟐
triangle is symmetrical about y axis
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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24. y y
x x
b/3
d/3 d/3
2b/3
b
d
b
d
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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25. SEMI CIRCLE
Let us consider a semi circular lamina of area (
𝝅𝑹 𝟐
𝟐
) as shown in Figure.
Now consider a triangular elementary strip of area (
𝟏
𝟐
x R x Rdθ) at an
angle of θ from the x-axis.
Its centre of gravity is
𝟐
𝟑
R from O.
its projection on the x-axis =
𝟐
𝟑
R cosθ
Moment of area of elementary strip about
the y-axis = (
𝟏
𝟐
x R x Rdθ) .
𝟐
𝟑
R cosθ
=
𝑹 𝟑 𝒄𝒐𝒔𝜽 d 𝜽
𝟑
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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27. QUATER CIRCLE
Let us consider a quarter circular lamina of area (
𝝅𝑹 𝟐
𝟒
) as shown in Figure.
Now consider a triangular elementary strip of area (
𝟏
𝟐
x R x Rdθ) at an
angle of θ from the x-axis.
Its centre of gravity is
𝟐
𝟑
R from O.
its projection on the x-axis =
𝟐
𝟑
R cosθ
Moment of area of elementary strip about
the y-axis = (
𝟏
𝟐
x R x Rdθ) .
𝟐
𝟑
R cosθ
=
𝑹 𝟑 𝒄𝒐𝒔𝜽 d 𝜽
𝟑
SERIN ISSAC, DEPARTMENT OF CIVIL ENGINEERING, NHCE
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