1 CM 197 Mechanics of Materials Chap 9: Strength of Materials Simple Stress Professor Joe Greene CSU, CHICO Reference: Statics and Strength of Materials,

Slides:



Advertisements
Similar presentations
Professor Joe Greene CSU, CHICO
Advertisements

Copyright Joseph Greene 2003 All Rights Reserved 1 CM 197 Mechanics of Materials Chap 16: Deflections of Beams Professor Joe Greene CSU, CHICO Reference:
3 Torsion.
Chapter Outline Shigley’s Mechanical Engineering Design.
CM 197 Mechanics of Materials Chap 8: Moments of Inertia
CTC / MTC 222 Strength of Materials Chapter 1 Basic Concepts.
2E4: SOLIDS & STRUCTURES Lecture 3 Dr. Bidisha Ghosh Notes: lids & Structures.
3 Torsion.
MAE 314 – Solid Mechanics Yun Jing
Chapter 6 Section 3,4 Bending Deformation, Strain and Stress in Beams
1 CM 197 Mechanics of Materials Chap 10: Strength of Materials Strains Professor Joe Greene CSU, CHICO Reference: Statics and Strength of Materials, 2.
CM 197 Mechanics of Materials Chap 14: Stresses in Beams
Professor Joe Greene CSU, CHICO
ENGR 225 Section
CM 197 Mechanics of Materials Chap 18: Combined Stresses
SWEDISH COLLEGE OF ENGINEERING & TECHNOLOGY
3 Torsion.
Copyright Joseph Greene 2003 All Rights Reserved 1 CM 197 Mechanics of Materials Chap 15: Design of Beams for Strength Professor Joe Greene CSU, CHICO.
Chapter 1 Stress.
MECHANICS OF MATERIALS 7th Edition
BSE 2294 Animal Structures and Environment
CHAPTER OBJECTIVES Review important principles of statics
Mechanics of Materials(ME-294)
CTC / MTC 222 Strength of Materials Final Review.
George F. Limbrunner and Leonard Spiegel Applied Statics and Strength of Materials, 5e Copyright ©2009 by Pearson Higher Education, Inc. Upper Saddle River,
1/1 SOE 1032 SOLID MECHANICS Website course organisation,lecture notes, tutorial.
EGR 280 Mechanics 6 – Introduction to Mechanics of Materials.
Strengths Chapter 10 Strains. 1-1 Intro Structural materials deform under the action of forces Three kinds of deformation Increase in length called an.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
Axial Members AXIAL MEMBERS, which support load only along their primary axis, are the most basic of structural members. Equilibrium requires that forces.
9 Torsion.
Chapter 1: Stress Review important principles of statics
Load and Stress Analysis
ENT 153 TUTORIAL 1.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
STRENGTHS Chapter Intro Dealing with relationship between the external loads applied to an elastic body and the intensity of the internal forces.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
Overview of Mechanical Engineering for Non-MEs Part 2: Mechanics of Materials 6 Introduction – Concept of Stress.
CTC / MTC 222 Strength of Materials Chapter 1 Basic Concepts.
3 Torsion.
Machine Design I (MCE-C 203) Mechatronics Dept., Faculty of Engineering, Fayoum University Dr. Ahmed Salah Abou Taleb Lecturer, Mechanical Engineering.
3 Torsion.
CTC / MTC 222 Strength of Materials Chapter 3 Design for Direct Stress.
Deformation of Axially Loaded Members - Single Member
Strength of Materials Malayer University Department of Civil Engineering Taught by: Dr. Ali Reza Bagherieh In The Name of God.
ENGR 107 – Introduction to Engineering Static Equilibrium, and Stress and Strain (Lecture #8)
MECHANICS OF MATERIALS Fourth Edition Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University CHAPTER.
1 MFGT 104 Materials and Quality Compression, Shear, Flexural, Impact Testing Professor Joe Greene CSU, CHICO.
Copyright Joseph Greene 2003 All Rights Reserved 1 CM 197 Mechanics of Materials Chap 17: Statically Indeterminate Beams Professor Joe Greene CSU, CHICO.
Mechanics of Elastic Materials. Why study mechanics? Useful for the analysis and design of load-bearing structures, such as: buildings bridges space shuttles.
Lecture 1 Stress 16 July 2007 ENT 450 Mechanics of Materials Dr. Haftirman 1 ENT 450 MECHANICS OF MATERIALS (MoM) RC. Hibbler Lecture: DR. HAFTIRMAN Teaching.
Stress and Strain1 Stress Analysis Mechanics: Stress and strain.
Mechanics of Solids (M2H321546)
Material Testing under Tension
Pure Bending.
Introduction – Concept of Stress
Concept of Stress.
3 Torsion.
Chapter 1 Stress and Strain.
3 Torsion.
Ch. 2: Fundamental of Structure
Structure I Course Code: ARCH 208 Dr. Aeid A. Abdulrazeg
Introduction – Concept of Stress
Units of N m.
3 Torsion.
Mechanics of Materials Engr Lecture 1
Concept of Stress.
Simple Stresses & Strain
CHAPTER OUTLINE Introduction Equilibrium of a deformable body Stress
1/1 SOE 1032 SOLID MECHANICS Website course organisation,lecture notes, tutorial.
Presentation transcript:

1 CM 197 Mechanics of Materials Chap 9: Strength of Materials Simple Stress Professor Joe Greene CSU, CHICO Reference: Statics and Strength of Materials, 2 nd ed., Fa-Hwa Cheng, Glencoe/McGraw Hill, Westerville, OH (1997) CM 197

2 Chap 9: Strength of Materials Simple Stress Objectives –Introduction –Normal and Shear Stresses –Direct Normal Stresses –Direct Shear Stresses –Stresses on an Inclined Plane

3 Introduction –Statics: first 8 chapters –Strength of Materials: Rest of book Relationships between external loads applied to an elastic body Intensity of the internal forces within the body Statics: all bodies are rigid. Strength of materials: all bodies are deformable –Terms Strain: deformation per unit length Stress: Force per unit area from an external source Strength: Amount of force per unit area that a material can support without breaking. Stiffness: A material’s resistance to deformation under load

4 Mechanical Test Considerations Normal and Shear Stresses –Force per unit area Normal force per unit area –Forces are normal (in same direction) to the surface Shear force per unit area –Forces are perpendicular (right angle) to the surface Direct Normal Forces and Primary types of loading –Prismatic Bar: bar of uniform cross section subject to equal and opposite pulling forces P acting along the axis of the rod. –Axial loads: Forces pulling on the bar –Tension= pulling the bar; Compression= pushing; torsion=twisting; flexure= bending; shear= sliding forces tension compression shear torsion flexure P P PPP P A

5 Stress Stress: Intensity of the internally distributed forces or component of forces that resist a change in the form of a body. –Tension, Compression, Shear, Torsion, Flexure Stress calculated by force, P, per unit area. Applied force divided by the cross sectional area of the specimen. –Note: P is sometimes called force, F.Eqn 9-1 Stress units –Pascals = Pa = Newtons/m 2 –Pounds per square inch = Psi Note: 1MPa = 1 x10 6 Pa = 145 psi –1 kPa = 10 3 Pa, 1 MPa = 106Pa, 1GPa = 109Pa –1 psi = 6.895kPa, 1ksi = 6.895MPa, 1 psf = Pa Example –Wire 12 in long is tied vertically. The wire has a diameter of in and supports 100 lbs. What is the stress that is developed? –Stress = P/A = P/  r 2 = 100/( * )= 12,739 psi = MPa

6 Stress Example –Tensile Bar is 10in x 1in x 0.1in is mounted vertically in test machine. The bar supports 100 lbs. What is the stress that is developed? What is the Load? Stress = F/A = F/(width*thickness) = 100lbs/(1in*.1in )= 1,000 psi = 1000 psi/145psi = MPa Load = 100 lbs –Block is 10 cm x 1 cm x 5 cm is mounted on its side in a test machine. The block is pulled with 100 N on both sides. What is the stress that is developed? What is the Load? Stress = F/A = F/(width*thickness) = 100N/(.01m *.10m )= 100,000 N/m 2 = 100,000 Pa = 0.1 MPa= 0.1 MPa *145psi/MPa = 14.5 psi Load = 100 N 10in 1 in 0.1 in 10cm 5cm 1 cm 100 lbs

7 Allowable Axial Load Structural members are usually designed for a limited stress level called allowable stress, which is the max stress that the material can handle. –Equation 9-1 can be rewritten Required Area –The required minimum cross-sectional area A that a structural member needs to support the allowable stress is from Equation 9-1 –Eqn 9-3 –Example 9-1 –Internal Axial Force Diagram Varaition of internal axial force along the length of a member can be detected by this The ordinate at any section of a member is equal to the value of the internal axial force of that section Example 9-2