PROBLEM 7.1 SOLUTION. σ = 5.49 ksi. τ = ksi

Similar documents
PROBLEM 7.31 SOLUTION. β = τ max = 36.4 MPa. Solve Probs. 7.5 and 7.9, using Mohr s circle.

Stress Transformation Equations: u = +135 (Fig. a) s x = 80 MPa s y = 0 t xy = 45 MPa. we obtain, cos u + t xy sin 2u. s x = s x + s y.

CHAPER THREE ANALYSIS OF PLANE STRESS AND STRAIN

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS

Module 2 Stresses in machine elements. Version 2 ME, IIT Kharagpur

MECHANICS OF MATERIALS Design of a Transmission Shaft

9. Stress Transformation

Spherical Pressure Vessels

MECHANICS OF MATERIALS

CHAPTER 4 Stress Transformation

MECE 3321 MECHANICS OF SOLIDS CHAPTER 1

Stress Analysis Lecture 3 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy

MECHANICS OF MATERIALS

CHAPTER 4: BENDING OF BEAMS

Validation of Stresses with Numerical Method and Analytical Method

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS Design of a Transmission Shaft

Principal Stresses, Yielding Criteria, wall structures

Samantha Ramirez, MSE. Stress. The intensity of the internal force acting on a specific plane (area) passing through a point. F 2

Mechanics of Materials Lab

2. Rigid bar ABC supports a weight of W = 50 kn. Bar ABC is pinned at A and supported at B by rod (1). What is the axial force in rod (1)?

Stress transformation and Mohr s circle for stresses

MECHANICS OF MATERIALS. Prepared by Engr. John Paul Timola

Aluminum shell. Brass core. 40 in

MECHANICS OF MATERIALS

Mechanics of Materials MENG 270 Fall 2003 Exam 3 Time allowed: 90min. Q.1(a) Q.1 (b) Q.2 Q.3 Q.4 Total

Unit IV State of stress in Three Dimensions

Determine the resultant internal loadings acting on the cross section at C of the beam shown in Fig. 1 4a.

The casing is subjected to the following:

ME 243. Lecture 10: Combined stresses

The hitch in all of this is figuring out the two principal angles and which principal stress goes with which principal angle.

STRESS. Bar. ! Stress. ! Average Normal Stress in an Axially Loaded. ! Average Shear Stress. ! Allowable Stress. ! Design of Simple Connections

UNIT-I Introduction & Plane Stress and Plane Strain Analysis

BTECH MECHANICAL PRINCIPLES AND APPLICATIONS. Level 3 Unit 5

Mohr's Circle for 2-D Stress Analysis

PROBLEM 5.1 SOLUTION. Reactions: Pb L Pa L. From A to B: 0 < x < a. Pb L Pb L Pb L Pbx L. From B to C: a < x < L Pa L. Pa L. L Pab At section B: M = L

FINAL EXAMINATION. (CE130-2 Mechanics of Materials)

Stress Analysis Lecture 4 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy

Torsion of Shafts Learning objectives

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 2 Stress & Strain - Axial Loading

ARC 341 Structural Analysis II. Lecture 10: MM1.3 MM1.13

MECHANICS OF MATERIALS

CHAPTER 2 Failure/Fracture Criterion

ME 202 STRENGTH OF MATERIALS SPRING 2014 HOMEWORK 4 SOLUTIONS

Bending Stress. Sign convention. Centroid of an area

both an analytical approach and the pole method, determine: (a) the direction of the

Solid Mechanics Homework Answers

2. Polar moment of inertia As stated above, the polar second moment of area, J is defined as. Sample copy

The aircraft shown is being tested to determine how the forces due to lift would be distributed over the wing. This chapter deals with stresses and

6. Bending CHAPTER OBJECTIVES

1 of 12. Given: Law of Cosines: C. Law of Sines: Stress = E = G

[5] Stress and Strain

CIV E 205 Mechanics of Solids II. Course Notes

COLUMNS: BUCKLING (DIFFERENT ENDS)

Downloaded from Downloaded from / 1

If the solution does not follow a logical thought process, it will be assumed in error.

R13. II B. Tech I Semester Regular Examinations, Jan MECHANICS OF SOLIDS (Com. to ME, AME, AE, MTE) PART-A

Advanced Structural Analysis EGF Cylinders Under Pressure

TORSION INCLUDING WARPING OF OPEN SECTIONS (I, C, Z, T AND L SHAPES)

ME325 EXAM I (Sample)

MECHANICS OF MATERIALS

IDE 110 Mechanics of Materials Spring 2006 Final Examination FOR GRADING ONLY

A concrete cylinder having a a diameter of of in. mm and elasticity. Stress and Strain: Stress and Strain: 0.

LIMITATIONS OF THE STANDARD INTERACTION FORMULA FOR BIAXIAL BENDING AS APPLIED TO RECTANGULAR STEEL TUBULAR COLUMNS

7. STRESS ANALYSIS AND STRESS PATHS

Mechanics of Materials

1 of 7. Law of Sines: Stress = E = G. Deformation due to Temperature: Δ

ME Final Exam. PROBLEM NO. 4 Part A (2 points max.) M (x) y. z (neutral axis) beam cross-sec+on. 20 kip ft. 0.2 ft. 10 ft. 0.1 ft.

MECHANICS OF MATERIALS

Chapter 5 CENTRIC TENSION OR COMPRESSION ( AXIAL LOADING )

Free Body Diagram: Solution: The maximum load which can be safely supported by EACH of the support members is: ANS: A =0.217 in 2

STRESS, STRAIN AND DEFORMATION OF SOLIDS

and F NAME: ME rd Sample Final Exam PROBLEM 1 (25 points) Prob. 1 questions are all or nothing. PROBLEM 1A. (5 points)

PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics

PROBLEM 3.3 ( )(45 10 ) T 5.17 kn m. A c c. 2 J c, (2)( ) 2 ( ) mm ( )

MAAE 2202 A. Come to the PASS workshop with your mock exam complete. During the workshop you can work with other students to review your work.

8. Combined Loadings

Solution ME 323 EXAM #2 FALL SEMESTER :00 PM 9:30 PM Nov. 2, 2010

VYSOKÁ ŠKOLA BÁŇSKÁ TECHNICKÁ UNIVERZITA OSTRAVA

Constitutive Equations (Linear Elasticity)

Endurance Strength Pg 274

MECE 3321: MECHANICS OF SOLIDS CHAPTER 5

Mechanical Properties of Materials

ENT345 Mechanical Components Design

SEMM Mechanics PhD Preliminary Exam Spring Consider a two-dimensional rigid motion, whose displacement field is given by

MTE 119 STATICS FINAL HELP SESSION REVIEW PROBLEMS PAGE 1 9 NAME & ID DATE. Example Problem P.1

Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on Exam 3.

Chapter 1 Introduction- Concept of Stress

This chapter is devoted to the study of torsion and of the stresses and deformations it causes. In the jet engine shown here, the central shaft links

CHAPTER 6: Shearing Stresses in Beams

Matlab Sheet 2. Arrays

Failure from static loading

(48) CHAPTER 3: TORSION

Chapter 3. Load and Stress Analysis. Lecture Slides

Internal Internal Forces Forces

3 A y 0.090

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 6 Shearing Stress in Beams & Thin-Walled Members

Transcription:

PROBLEM 7.1 For the given state of stress, determine the normal and shearing stresses exerted on the oblique face of the shaded triangular element shon. Use a method of analysis based on the equilibrium of that element, as as done in the derivations of Sec. 7.. Stresses Areas Forces F = : σ A 15 A sin 3 cos 3 15 A cos 3 sin 3 + 1 A cos 3 cos 3 = σ = 3 sin 3 cos 3 1 cos 3 Σ F = : τ A+ 15 A sin 3 sin 3 15 A cos 3 cos 3 1 A cos 3 sin 3 = τ = 15(cos 3 sin 3 ) + 1 cos 3 sin 3 σ = 5.49 ksi τ = 11.83 ksi PROPRIETARY MATERIAL. 1 The McGra-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed,

PROBLEM 7.4 For the given state of stress, determine the normal and shearing stresses exerted on the oblique face of the shaded triangular element shon. Use a method of analysis based on the equilibrium of that element, as as done in the derivations of Sec. 7.. Stresses Areas Forces Σ F = : σ A+ 18 A cos 15 sin 15 + 45 A cos 15 cos 15 7 A sin 15 sin 15 + 18 A sin 15 cos 15 = σ = 18 cos 15 sin 15 45 cos 15 + 7sin 15 18 sin 15 cos 15 σ = 49. MPa Σ F = : τ A+ 18 A cos 15 cos 15 45 A cos 15 sin 15 7 A sin 15 cos 15 18 A sin 15 sin 15 = τ = 18(cos 15 sin 15 ) + (45 + 7) cos 15 sin 15 τ =.41 MPa PROPRIETARY MATERIAL. 1 The McGra-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed,

PROBLEM 7.5 For the given state of stress, determine (a) the principal planes, (b) the principal stresses. σ = MPa σ = 4 MPa τ = 35 MPa x y xy (a) τ xy ()(35) tan θ p = 3.5 σ σ = + 4 = x y θ p = 74.5 θ p = 37., 53. (b) σ max, min σx + σy σx σy = ± + τ xy 4 + 4 = ± + (35) = 5 ± 3.4 MPa σ = 13. MPa max σ = 8.4 MPa min PROPRIETARY MATERIAL. 1 The McGra-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed,

PROBLEM 7.8 For the given state of stress, determine (a) the principal planes, (b) the principal stresses. σ = 8ksi σ = 1ksi τ = 5ksi x y xy (a) τ xy (5) tan θ p = =.5 σ σ 8 1 = x y θ p =.551 θ p = 13.3, 7.7 (b) σ max, min σx + σy σx σ y = ± + τ xy 8 + 1 8 1 = ± + (5) = ± 11.183 σ max = 13.18 ksi σ min = 9.18 ksi PROPRIETARY MATERIAL. 1 The McGra-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed,

PROBLEM 7.19 A steel pipe of 1-in. outer diameter is fabricated from 1 -in.-thick plate by 4 elding along a helix that forms an angle of.5 ith a plane perpendicular to the axis of the pipe. Knoing that a 4-kip axial force P and an 8-kip in. torque T, each directed as shon, are applied to the pipe, determine σ and τ in directions, respectively, normal and tangential to the eld. Stresses: 1 d = 1 in., c = d = in., t =.5 in. c = c t = 5.75 in. 1 ( 1 ) ( 1 ) A= π c c = π( 5.75 ) = 9.84 in π π J = c c = ( 5.75 ) = 318.7 in 4 4 4 4 4 P σ = A 4 = = 4.3344 ksi 9.84 Tc τ = J (8)() = = 1.53 ksi 318.7 σ =, σ = 4.3344 ksi, τ = 1.53 ksi x y xy Choose the x and y axes, respectively, tangential and normal to the eld. Then σ = σ and τ = τ θ =.5 y xy σx + σy σx σ y σy = cos θ τxysin θ ( 4.3344) [ ( 4.3344)] = cos 45 1.53 sin 45 = 4.7 ksi σ = 4.7 ksi σx σy τxy = sin θ + τxycos θ [ ( 4.3344)] = sin 45 + 1.53 cos45 =.47 ksi τ =.47 ksi PROPRIETARY MATERIAL. 1 The McGra-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed,

PROBLEM 7. To steel plates of uniform cross section 1 8 mm are elded together as shon. Knoing that centric 1-kN forces are applied to the elded plates and that the in-plane shearing stress parallel to the eld is 3 MPa, determine (a) the angle β, (b) the corresponding normal stress perpendicular to the eld. Area of eld: A = = 3 3 (1 1 )(8 1 ) cos β 8 1 cos β m (a) (b) F = : F 1sin β = F = 1sin β kn = 1 1 sin β N s s s 3 1 1 sin β Fs τ = 3 1 = = 15 1 sin βcos β A 8 1 / cos β 1 3 1 sin βcos β = sin β = =.4 15 1 F = : F 1cosβ = F = 1cos14.34 = 9.88 kn A n n n 8 1 = = 85.74 1 m cos14.34 3 Fn 9.88 1 σ = = = 117.3 1 Pa A 85.74 1 3 β = 14.34 σ = 117.3 MPa PROPRIETARY MATERIAL. 1 The McGra-Hill Companies, Inc. All rights reserved. No part of this Manual may be displayed,