Triaxial State of Stress at any Critical Point in a Loaded Body

Slides:



Advertisements
Similar presentations
Stress in any direction
Advertisements

Overview of Loads ON and IN Structures / Machines
Mechanics of Materials – MAE 243 (Section 002) Spring 2008
Chapter 6 Bending.
Read Chapter 1 Basic Elasticity - Equilibrium Equations
Chapter Outline Shigley’s Mechanical Engineering Design.
BIBLIOGRAFIA de referencia
Hamrock Fundamentals of Machine Elements Chapter 2: Load, Stress and Strain The careful text-books measure (Let all who build beware!) The load, the shock,
MAE 314 – Solid Mechanics Yun Jing
PLANE STRESS TRANSFORMATION
CHAPTER OBJECTIVES Apply the stress transformation methods derived in Chapter 9 to similarly transform strain Discuss various ways of measuring strain.
Copyright © 2011 Pearson Education South Asia Pte Ltd
CTC / MTC 222 Strength of Materials
Principle and Maximum Shearing Stresses ( )
Analysis of Stress and Strain
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
Analysis of Stress and Strain Review: - Axially loaded Bar - Torsional shaft Questions: (1) Is there any general method to determine stresses on any arbitrary.
Stress Transformation
ENGR 220 Section
Chapter Outline Shigley’s Mechanical Engineering Design.
Beams Beams: Comparison with trusses, plates t
Chapter 2: Load, Stress and Strain
Mechanics of Materials(ME-294)
Stress II Cauchy formula Consider a small cubic element of rock extracted from the earth, and imagine a plane boundary with an outward normal, n, and an.
Ken Youssefi Mechanical Engineering Department 1 Normal & Shear components of stress Normal stress is perpendicular to the cross section,  (sigma). Shear.
Bending Shear and Moment Diagram, Graphical method to construct shear
MECHANICS OF MATERIALS 7th Edition
Theories of Stress and Strain
MAE 343-Intermediate Mechanics of Materials QUIZ No.1 - Thursday, Aug. 26, 2004 List three possible failure modes of a machine element (5points) List the.
Content Stress Transformation A Mini Quiz Strain Transformation
Load and Stress Analysis
Transformations of Stress and Strain
APPLICATIONS/ MOHR’S CIRCLE
8 Principle Stresses Under a Given Loading. © 2002 The McGraw-Hill Companies, Inc. All rights reserved. MECHANICS OF MATERIALS ThirdEdition Beer Johnston.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
If A and B are on the same side of the origin (i. e
1 Principal stresses/Invariants. 2 In many real situations, some of the components of the stress tensor (Eqn. 4-1) are zero. E.g., Tensile test For most.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
Introduction Stress: When some external system of forces act on a body, the internal forces are set up at various sections of the body, which resist the.
Main Steps of Beam Bending Analysis Step 1 – Find Reactions at External Supports –Free Body Diagram (FBD) of Entire Beam –Equations of Force and Moment.
CHAPTER OBJECTIVES To show how to transform the stress components that are associated with a particular coordinate system into components associated with.
Stress and Strain ( , 3.14) MAE 316 – Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering Stress.
Transformations of Stress and Strain
1 INTRODUCTION The state of stress on any plane in a strained body is said to be ‘Compound Stress’, if, both Normal and Shear stresses are acting on.
MOHR'S CIRCLE The formulas developed in the preceding article may be used for any case of plane stress. A visual interpretation of them, devised by the.
CTC / MTC 222 Strength of Materials
CHAPTER OBJECTIVES Derive equations for transforming stress components between coordinate systems of different orientation Use derived equations to.
6. Strain Assoc.Prof.Dr. Ahmet Zafer Şenalp Mechanical Engineering Department Gebze Technical University.
Transformation methods - Examples
Principal Stresses and Strain and Theories of Failure
Conclusions on Transverse Shearing Stress Calculations Maximum Value at Neutral Axis – IF CROSS- SECTION IS NOT NARROWER ELSEWHERE –Depends on Shape of.
1. PLANE–STRESS TRANSFORMATION
DEPARTMENT OF MECHANICAL AND MANUFACTURING ENGINEERING
Overview Introduction
Stress in any direction
Mohr’s circle for plane stress
If A and B are on the same side of the origin (i. e
Pure Bending.
Transformations of Stress and Strain
Transformations of Stress and Strain
CTC / MTC 222 Strength of Materials
ES2501: Statics/Unit 20-1: Internal Forces in Beams
CHAPTER OBJECTIVES Derive equations for transforming stress components between coordinate systems of different orientation Use derived equations to.
BDA30303 Solid Mechanics II.
Example 7.01 SOLUTION: Find the element orientation for the principal stresses from Determine the principal stresses from Fig For the state of plane.
Ch. 2: Fundamental of Structure
Copyright ©2014 Pearson Education, All Rights Reserved
Compound Normal & Shear Stresses
Copyright ©2014 Pearson Education, All Rights Reserved
Copyright ©2014 Pearson Education, All Rights Reserved
Presentation transcript:

Triaxial State of Stress at any Critical Point in a Loaded Body Cartesian stress components are found first in selected x-y-z coordinate axes (Fig. 4.1) Three mutually perpendicular principal planes are found at unique orientations: NO Shear stresses on these planes Principal Normal Stresses: 1, 3, 2, one of which is maximum normal stress at the point Three mutually perpendicular Principal Shearing Planes (Planes of max. shear) Principal Shearing Stresses: 1, 2, 3, one of which is the maximum shear stress at the point Normal stresses are NOT zero, NOT principal stresses and depend on the type of loading

3-D Stress Transformations Equations Relate Known Cartesian Stress Components at Any Point with Unknown Stress Components on Any Other Plane through the SAME Point From equilibrium conditions of infinitesimal pyramid Important for the Unique Orientations of the Principal Normal and Shearing Planes Stress Cubic Equation- three real roots are the Principal Normal Stresses, 1, 2, 3. Principal Shearing Stresses can be calculated from the Principal Normal Stresses as follows:

Mohr’s Circle Analogy for Stress – Graphical Transformation of 2-D Stress State Principal stress solution of stress cube eq. for stresses in the x-y plane (Fig. 4.12) Analogy with the equation of a circle plotted in the - plane leads to Mohr’s circle for biaxial stress: Sign convention for plotting the Mohr’s circle (normal stress is positive for tension, shear is positive for clockwise (CW) couple) Two additional Mohr’s circle for triaxial stress states Find orientation of principal axes from the Mohr’s circle

Strain Cubic Equation and Principal Strains STRAIN – a measure of loading severity, defining the intensity and direction of deformation at a point, w.r.t. specified planes through that point. Strain state at a point is completely defined by: Three normal and three shearing strain components in the selected x-y-z coordinate system, OR Three PRINCIPAL strains and their directions from Strain Cubic Equation (similar to Stress Cubic Equation, where ’s are replaced by ’s, and shear stresses, ’s, are replaced by one-half of ’s.)

Summary of Example Problems Example 4.8 – Principal Stresses in Beam Hollow cylindrical member subjected to transverse forces (four-point bending), axial force and torque Sketch state of stress at critical point (bottom edge) Use “stress cubic equation” to find principal stresses from calculated Cartesian stresses at critical point Find principal shear stresses from principal normal ones Example 4.9 –Mohr’s Circle for Stress Semi-graphical analysis of biaxial stress state at critical point of previous example cube is replaced by 2-D sketch in x-y plane Principal normal and shear stresses are found graphically from the basic and the two additional Mohr circles, respectively

Summary of Textbook Problems – Problem 4.31, Principal Stresses Identify critical points for each of the three types of loading applied on the bar Locations where stresses are amplified by superposition of effects from different loads – top end of vertical diameter and left end of horizontal one Sketch infinitesimal cube elements for the states of stress at critical points Calculate stresses at critical points, in the given system of Cartesian coordinates Use “stress cubic equation” to find the principal stresses at each of the two critical points Top edge: 1=26,047 psi, 2=0, 3=-7683 psi Left edge: 1=31,124 psi, 2=0, 3=-31,124 psi Calculate the maximum shearing stress at each point Top edge: max= 16,865 psi, while at the left edge: max= 31,124 psi