The beam shown in Fig. 3 carries a concentrated load of W and a total U.D.L load of 8 Determine the maximum safe value W that will not exceed allowable stresses provided in the below. Group 0.(MPa) 0.(MPa) T(MPa) 15 58 18 64 12 22 72 16 26 84 22 E 30 92 26 F 32 98 32 Im sw 2 m Im RI R2 200 (Fig. 3) est

The beam shown in Fig. 3 carries a concentrated load of W and a total U.D.L load of 8 Determine the maximum safe value W that will not exceed allowable stresses provided in the below. Group 0.(MPa) 0.(MPa) T(MPa) 15 58 18 64 12 22 72 16 26 84 22 E 30 92 26 F 32 98 32 Im sw 2 m Im RI R2 200 (Fig. 3) est

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 1.5.3P: A tensile test was performed on a metal specimen having a circular cross section with a diameter 0....

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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.
2) A solid rod with the given dimension shown in Fig. Axial loads are applied at the positions indicated. Find the f a) The max Compressive stress in the system P-60 kN Aluminum A=400 mm b) The max Tensile stress in the system P-60 kN Steel A = 500 mm² Bronze A-200 mm² 4P 2.5 m 1.5 m 2.0 m 2P
Q # 4: An aluminum rod is rigidly attached between a steel rod and a bronze rod as shown in Figure. Axial loads are applied at the positions indicated. The value of P is limited to 20 KN in bronze, 72 KN in aluminum and 28 KN in steel Find the area of each section that will not exceed a stress in steel of 280 MPa, in aluminum of 180 MPa, or in bronze of 200 MPa. CLO -2 Steel Aluminum Bronze 2P 4P 2.5 2.0 1.5
1/2 Problem 1: Two solid cylindrical rods AB and BC are welded together at B and loaded as shown in. If the stress must not exceed 14OMPA in either rod, determine the smallest allowable value of the diameter of rod AB and ВС. 300mm B 40 kN 250mm - d2 30 kN
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
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
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
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
A uniform bar 1 is connected to a tapered rod 2. Both are subjected to aodal loads as shown. If P-7 IN, Determine the total aodal deformation (in mm). Indicate negative sign f comoression. @ 5P O 3P E-200 6P 30 mm emm 80 mm 30 mn 30 mm
ed-fixed NOTE Do not continue to load the struts after the buckling load has been reached otherwise the struts will become permanently deformed! Enter your results into Table 3. TUAT2 Strut Length Buckling load 1/L2 number (m2) 12,75 918 6,92 (mm) (N) -344 - 275 -195 - 154 - 119 PHE 1 280 330 380 4. 430 OFS 4,34 Table 3 Results for experiment 2 (fixed-fixed) 480 Plot separate graphs of buckling load versus 1/L and calculate the gradient of each line. Establish ratios between each end condition (taking the pinned-pinned condition as 1). Examine the Euler buckling formulae for each end condition and confirm that the experimental and theoretical ratios are similar.
A ngid bar AB is hinged at A and is supported by a rod CD at C. The rod is pin connected at D. as shown Neglect deflections of the bar due to bending Use E200 GPa What is the displacement of the loaded end of the bar? 2 Determine the tensile stress induced in rod CD by the 80 kN load the alowable stress in rod CD is 124 MPa, what weight W can be safely applied?
Aluminum Bronze Steel 2P 3P P 4P - - 1.0 m 0.8 m FIG. P2.16 2.16 A compound bar consisting of bronze, aluminum, and steel segments is loaded axially as shown in the figure. Determine the maximum allowable value of P if the change in length of the bar is limited to 2 mm and the working stresses pre- scribed in the table are not to be exceeded. A (mm²) E (GPa) G, (MPa) Вronze 450 83 120 Aluminum 600 70 80 Steel 300 200 140