For the following problem please show intermediate steps including free body diagrams, equations used, and problem setup so your approach can be followed. (Problem 2.T28 from the text book) The specimen shown is made from a 1-in.-diametercylindrical steel rod with two 1.5-in.-outer-diameter sleeves bonded to the rod as shown.Knowing thatE=29 x 10° psi, determine (a) the load P so that the total deformation is 0.002in., (b) the corresponding deformation of the central portion BC..%3D1-in. diameter1-in. diameter1-in. diameter2 in.3 in,54°F Sunny

Answered: Image /qna-images/answer/d3248dd4-8435-4bd7-a7e9-acb7e51bd137.jpg

Answered: Knowing thatE=29 x 10° psi, determine…

Knowing thatE=29 x 10° psi, determine (a) the load P so that the total deformation is 0.002 in.. (b) the corresponding deformation of the central portion BC..

Steel Design (Activate Learning with these NEW titles from Engineering!)

6th Edition

ISBN:9781337094740

Author:Segui, William T.

Publisher:Segui, William T.

Chapter1: Introduction

Section: Chapter Questions

Problem 1.5.4P: A tensile test was performed on a metal specimen with a diameter of 1 2 inch and a gage length (the...

See similar textbooks

Similar questions

A tensile test was performed on a metal specimen having a circular cross section with a diameter 0. 510 inch. For each increment of load applied, the strain was directly determined by means of a strain gage attached to the specimen. The results are, shown in Table: 1.5.1. a. Prepare a table of stress and strain. b. Plot these data to obtain a stress-strain curve. Do not connect the data points; draw a best-fit straight line through them. c. Determine the modulus of elasticity as the slope of the best-fit line.
A tensile test was performed on a metal specimen with a diameter of 1 2 inch and a gage length (the length over which the elongation is measured) of 4 inches. The dam were plotted on a load-displacement graph. P vs. L. A best-fit line was drawn through the points, and the slope of the straight-line portion was calculated to be P/L =1392 kips/in. What is the modulus of elasticity?
2.17 The specimen shown has been cut from a -in.-thick sheet of vinyl (E = 0.45 × 10 psi) and is subjected to a 350-lb tensile load. Determine (a) the total deformation of the specimen, (b) the deformation of its central portion BC. B 0.4 in. C D P = 350 lb P = 350 lb 1 in. 1 in. -1.6 in.---2 in. -1.6 in-
PROBLEM 1) An aluminum bar carries the axial loads at the positions shown. If E=70GPA, compute the total deformation of the bar. Assume that the bar is suitably braced to prevent buckling. 0.4m D 10KN 6) What is the deformation &c in mm? 0.8m 0.4m B 5KN 0.6m 20KN A=800 mm? A=1,200 mm²
An aluminum bar carries the axial loads at the positions shown. If E=70GPA, compute the total deformation of the bar. Assume that the bar is suitably braced to prevent buckling. 0.4m 10KN 0.8m 0.4m 5KN 0.6m What is the deformation 8Rc in mm? Al 20KN A=800 mm? A=1,200 mm²
PROBLEM 1) An aluminum bar carries the axial loads at the positions shown. If E=70GPA, compute the total deformation of the bar. Assume that the bar is suitably braced to prevent buckling. 0.4m D 10KN. 0.8m 0.4m B 5KN 0.6m Al 20KN Q2 5) What is the deformation 8, in mm? A=800 mm? A=1,200 mm?
The shown plate is 60 mm thick and it is made of Magnesium Am1004-T61. The plate is fitted between the rigid frictionless supports as shown and at T, = 20°C it is stress free. Find the stresses in the x and y directions when the temperature increases to T, = 58°C. %3D 150 mm 150 mm Select one: O x: 0 MPa, y: 42.864 MPa Ox: 22.1 MPa, y: 44.2 MPa Ox: 0 MPa, y: 44.2 MPa Ox: 0 MPa, y: 17.8 MPa O x: 13.2 MPa, y: 44.2 MPa Ox: 0 MPa, y: 67.4 MPa 3:10 PM O G 4) ENG 1/31/2021
13- is defined as deformations not only cause line segments to elongate or contract, but they also cause them to change direction. A)Normal Strain B) Normal Stress C) Shear strain The normal strains cause a change in --- B) shape The shear strains cause a change in its shape. 14- A)Direction C) volume 15- C) volume -- by dividing the applied load P by the A)Direction We can determine the --- specimen's original cross-sectional area Ap. A)engineering stress B) True stress B) shape 16- C) Engineering strain D) True strain 17- is found directly from the strain gauge reading, or by ------------- dividing the change in the specimen's gauge length, 8, by the specimen's original gauge length Lo. A)Engineering stress B) True stress C) Engineering strain D) True strain 18- Any material that can be subjected to large strains before it fractures is called a---------- A)Brittle material B) Soft material C) Ductile material
PROBLEM 1) An aluminum bar carries the axial loads at the positions shown. If E=70GPA, compute the total deformation of the bar. Assume that the bar is suitably braced to prevent buckling. 0.4m D 10KN 0.8m 0.4m B 5KN 0.6m AL 20KN What is the deformation &pE in mm? A=800 mm² A=1,200 mm²
PROBLEM 1) An aluminum bar carries the axial loads at the positions shown. If E=70GPA, compute the total deformation of the bar. Assume that the bar is suitably braced to prevent buckling. 0.4m D What is the axial stress o Ag in Pa? 10KN 0.8m 0.4m B 5KN 0.6m 20KN A=800 mm? A=1,200 mm²
The state of plane stress shown occurs at a critical point of a steel machine component. As a result of several tensile tests, it has been found that the tensile yield strength is o, = 250 MPa for the grade of steel used. Determine the factor of safety with respect to yield using (a) the maximum shearing stress criterion, and (b) the maximum distortion energy criterion. ↑y 40 40 MPa 80 MPa 25 MPa ➜X
Q3: For the assembly shown in Fig. Q3. Axial loads are applied at the positions indicated. Find the largest value of P that will not exceed an overall deformation of 3.0 mm, or the following stresses: 140 MPa in the steel, 120 MPa in the bronze, and 80 MPa in the aluminum. Steel Bronze Aluminum B C A D P ЗР 4P +2P | 1m 2m 1.5m A= 480 mm? A= 650 mm? A= 320 mm? E= 200 GPa E= 83 GPa E= 70 GPa Fig. Q3