Stress and Strain (3.8-3.12, 3.14) MAE 316 – Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering Stress.

Slides:



Advertisements
Similar presentations
Sample Problem 4.2 SOLUTION:
Advertisements

Definition I. Beams 1. Definition
1 Thin Walled Pressure Vessels. 2 Consider a cylindrical vessel section of: L = Length D = Internal diameter t = Wall thickness p = fluid pressure inside.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008
Course Title: Strength of Materials (CVE 202)
4 Pure Bending.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
Beams and Frames.
Copyright Joseph Greene 2003 All Rights Reserved 1 CM 197 Mechanics of Materials Chap 16: Deflections of Beams Professor Joe Greene CSU, CHICO Reference:
Chapter Outline Shigley’s Mechanical Engineering Design.
Strength of Materials I EGCE201 กำลังวัสดุ 1
MAE 314 – Solid Mechanics Yun Jing
CHAPTER 6 BENDING.
Chapter 6 Section 3,4 Bending Deformation, Strain and Stress in Beams
Load and Stress Analysis
Principle and Maximum Shearing Stresses ( )
Combined Loadings Thin-Walled Pressure Vessels Cylindrical Pressure VesselSpherical Pressure Vessel.
4 Pure Bending.
Plastic Deformations of Members With a Single Plane of Symmetry
Copyright © 2011 Pearson Education South Asia Pte Ltd
Beams: Pure Bending ( ) MAE 314 – Solid Mechanics Yun Jing Beams: Pure Bending.
Chapter Outline Shigley’s Mechanical Engineering Design.
Contact Stress (3.19) MAE 316 – Strength of Mechanical Components
Beams Beams: Comparison with trusses, plates t
AE2302 AIRCRAFT STRUCTURES-II
10 Pure Bending.
Chapter 4: Stresses and Strains
CHAPTER OBJECTIVES Determine stress in members caused by bending
Mechanics of Materials Goal:Load Deformation Factors that affect deformation of a structure P PPP Stress: intensity of internal force.
BFC (Mechanics of Materials) Chapter 3: Stress in Beam
Beams Session Subject: S1014 / MECHANICS of MATERIALS Year: 2008.
Plastic Deformations of Members With a Single Plane of Symmetry
CHAPTER OBJECTIVES Analyze the stress developed in thin-walled pressure vessels Review the stress analysis developed in previous chapters regarding axial.
CTC / MTC 222 Strength of Materials Final Review.
Lecture 5-6 Beam Mechanics of Materials Laboratory Sec. 3-4 Nathan Sniadecki University of Washington Mechanics of Materials Lab.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008
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.
9 Torsion.
Load and Stress Analysis
 2005 Pearson Education South Asia Pte Ltd 7. Transverse Shear 1 CHAPTER OBJECTIVES Develop a method for finding the shear stress in a beam having a prismatic.
Pure Bending of Straight Symmetrical Beams
CHAPTER OBJECTIVES Analyze the stress developed in thin-walled pressure vessels Review the stress analysis developed in previous chapters regarding axial.
Chapter 4 Pure Bending Ch 2 – Axial Loading Ch 3 – Torsion
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
Shear Stress in Beams ( )
Strength of Materials Outline Overview AXIALLY LOADED MEMBERS THIN-WALLED CYLINDER GENERAL STATE OF STRESS PLANE STRESS + MOHR’S CIRCLE PLANE STRAIN +
3 Torsion.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008
Forging new generations of engineers
Mechanics of Materials(ME-294)
COMBINED LOADING.  Analyze the stress developed in thin-walled pressure vessels  Review the stress analysis developed in previous chapters regarding.
☻ 2.0 Bending of Beams sx 2.1 Revision – Bending Moments
Copyright Kaplan AEC Education, 2005 Mechanics of Materials Outline Overview AXIALLY LOADED MEMBERS, p. 262 Modulus of Elasticity Poisson’s Ratio Thermal.
Chapter 4 Pure Bending Ch 2 – Axial Loading Ch 3 – Torsion Ch 4 – Bending -- for the designing of beams and girders.
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 6: Bending.
EGM 5653 Advanced Mechanics of Materials
Combined Loadings Thin-Walled Pressure Vessels Stress caused by Combined Loadings.
 2005 Pearson Education South Asia Pte Ltd 6. Bending 1 CHAPTER OBJECTIVES To determine stress in members caused by bending To discuss how to establish.
BME 315 – Biomechanics Chapter 4. Mechanical Properties of the Body Professor: Darryl Thelen University of Wisconsin-Madison Fall 2009.
Longitudinal Strain Flexure Formula
Pure Bending.
Thin Walled Pressure Vessels
Ch. 2: Fundamental of Structure
326MAE (Stress and Dynamic Analysis) 340MAE (Extended Stress and Dynamic Analysis)
Structure I Course Code: ARCH 208 Dr. Aeid A. Abdulrazeg
Theory of Simple Bending
Chapter 6 Bending.
Forging new generations of engineers
Copyright ©2014 Pearson Education, All Rights Reserved
Presentation transcript:

Stress and Strain (3.8-3.12, 3.14) MAE 316 – Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering Stress and Strain

Introduction MAE 316 is a continuation of MAE 314 (solid mechanics) Review topics Beam theory Columns Pressure vessels Principle stresses New topics Contact Stress Press and shrink fits Fracture mechanics Fatigue Stress and Strain

Normal Stress (3.9) Normal Stress (axial loading) Sign Convention σ > 0 Tensile (member is in tension) σ < 0 Compressive (member is in compression) Stress and Strain

Shear Stress (3.9) Shear stress (transverse loading) “Single” shear “Double” shear average shear stress Stress and Strain

Stress and Strain Review (3.3) Bearing stress Bearing stress is a normal stress Single shear case Stress and Strain

Where E = Modulus of Elasticity (Young’s modulus) Strain (3.8) Normal strain (axial loading) Hooke’s Law Where E = Modulus of Elasticity (Young’s modulus) Stress and Strain

Stress and Strain Review (3.12) Torsion (circular shaft) Shear strain Shear stress Angle of twist T Where G = Shear modulus (Modulus of rigidity) and J = Polar moment of inertia of shaft cross-section Stress and Strain

Thin-Walled Pressure Vessels (3.14) Cylindrical Spherical Circumferential “hoop” stress Longitudinal stress Stress and Strain

Beams in Bending (3.10) Beams in pure bending Strain Stress Where ν = Poisson’s Ratio and ρ = radius of curvature Where I = 2nd moment of inertia of the cross-section Stress and Strain

Beam Shear and Bending (3.10-3.11) Beams (non-uniform bending) Shear and bending moment Shear stress Design of beams for bending Where Q = 1st moment of the cross-section Stress and Strain

Example Draw the shear and bending-moment diagrams for the beam and loading shown. Stress and Strain

Example Problem An extruded aluminum beam has the cross section shown. Knowing that the vertical shear in the beam is 150 kN, determine the shearing stress a (a) point a, and (b) point b. Shear Stress in Beams

Combined Stress in Beams In MAE 314, we calculated stress and strain for each type of load separately (axial, centric, transverse, etc.). When more than one type of load acts on a beam, the combined stress can be found by the superposition of several stress states. Stress and Strain

Combined Stress in Beams Determine the normal and shearing stress at point K. The radius of the bar is 20 mm. Stress and Strain

2D and 3D Stress (3.6-3.7) MAE 316 – Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering Stress and Strain

Plane (2D) Stress (3.6) Consider a state of plane stress: σz = τxz = τyz = 0. φ φ φ φ φ φ φ φ Slice cube at an angle φ to the x-axis (new coordinates x’, y’) φ Stress and Strain

Plane (2D) Stress (3.6) Sum forces in x’ direction and y’ direction and use trig identities to formulate equations for transformed stress. φ φ φ φ φ Stress and Strain

Plane (2D) Stress (3.6) Plotting a Mohr’s Circle, we can also develop equations for principle stress, maximum shearing stress, and the orientations at which they occur. Stress and Strain

Plane (2D) Strain Mathematically, the transformation of strain is the same as stress transformation with the following substitutions. Stress and Strain

3D Stress (3.7) Now, there are three possible principal stresses. Also, recall the stress tensor can be expressed in matrix form. Stress and Strain

3D Stress (3.7) We can solve for the principle stresses (σ1, σ2, σ3) using a stress cubic equation. Where i = 1,2,3 and the three constant I1, I2, and I3 are expressed as follows. Stress and Strain

3D Stress Let nx, ny and nz be the direction cosines of the normal vector to surface ABC with respect to x, y, and z directions respectively. Stress and Strain

3D Stress (3.7) How do we find the maximum shearing stress? The most visual method is to observe a 3D Mohr's Circle. Rank principle stresses largest to smallest: σ1 > σ2 > σ3 σ3 σ1 σ2 Stress and Strain

3D Stress (5.5) A plane that makes equal angles with the principal planes is called an octahedral plane. Stress and Strain

3D Stress (3.7) For the stress state shown below, find the principle stresses and maximum shear stress. Stress tensor Stress and Strain

3D Stress (3.7) Draw Mohr’s Circle for the stress state shown below. Stress tensor Stress and Strain

Curved Beams (3.18) MAE 316 – Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering Stress and Strain

Curved Beams (3.18) Thus far, we have only analyzed stress in straight beams. However, there many situations where curved beams are used. Hooks Chain links Curved structural beams Stress and Strain

Curved Beams (3.18) Assumptions What does this mean? Pure bending (no shear and axial forces present – will add these later) Bending occurs in a single plane The cross-section has at least one axis of symmetry What does this mean? σ = -My/I no longer applies Neutral axis and axis of symmetry (centroid) are no longer the same Stress distribution is not linear Stress and Strain

Curved Beams (3.18) Flexure formula for tangential stress: Where M = bending moment about centroidal axis (positive M puts inner surface in tension) y = distance from neutral axis to point of interest A = cross-section area e = distance from centroidal axis to neutral axis rn = radius of neutral axis Stress and Strain

Curved Beams (3.18) If there is also an axial force present, the flexure formula can be written as follows. Table 3-4 in the textbook shows rn formulas for several common cross-section shapes. Stress and Strain

Example Plot the distribution of stresses across section A-A of the crane hook shown below. The cross section is rectangular, with b=0.75 in and h =4 in, and the load is F = 5000 lbf. Stress and Strain

Curved Beams (3.18) Calculate the tangential stress at A and B on the curved hook shown below if the load P = 90 kN. Stress and Strain