The two bars are made of polystyrene, which has thestress-strain diagram shown in the figure below. The barsrupture simultaneously when the load P = 13.5 kN isapplied. Assume that buckling does not occur(Figure 1)(Figure 2)Part ADetermine the cross-sectional area of bar BC.Express your answer to three significant figures and include the appropríate units.ABC = 10.4m-SubmitPrevious Answers Request AnswerFigure< 2 of 2 >X Incorrect; Try Again; 5 attempts remaining(MPa)Part B175Determine the cross-sectional area of bar AB.140Express your answer to three significant figures and include the appropriate units.105compression70HÀ35- tensione (mm/mm)0.200.400.600.80AAB = 8.65mSubmitPrevious Answers Request Answer The two bars are made of polystyrene, which has thestress-strain diagram shown in the figure below The barsrupture simultaneously when the load P = 13.5 kN isapplied Assume that buckling does not occur(Figure 1)(Figure 2)Part ADetermine the cross-sectional area of bar BC.Express your answer to three significant figures and include the appropriate units.ABC = 10.4mSubmitPrevious Answers Request AnswerFigure1 of 2X Incorrect; Try Again; 5 attempts remainingPart B-1.2 mDetermine the cross-sectional area of bar ABExpress your answer to three significant figures and include the appropriate units.1mHAAAB = 8.65m

The two bars are made of polystyrene, which has the stress-strain diagram shown in the figure below. The bars rupture simultaneously when the load P = 13.5 kN is applied Assume that buckling does not occur (Figure 1) (Figure 2) Part A Determine the cross-sectional area of bar BC Express your answer to three significant figures and include the appropriate units. HA ApC = 10.4 m Submit Previous Answers Request Answer Figure < 2 of 2 > X Incorrect; Try Again; 5 attempts remaining (MPa) Part B

The two bars are made of polystyrene, which has the stress-strain diagram shown in the figure below. The bars rupture simultaneously when the load P = 13.5 kN is applied Assume that buckling does not occur (Figure 1) (Figure 2) Part A Determine the cross-sectional area of bar BC Express your answer to three significant figures and include the appropriate units. HA ApC = 10.4 m Submit Previous Answers Request Answer Figure < 2 of 2 > X Incorrect; Try Again; 5 attempts remaining (MPa) Part B

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

A round steel alloy bar with a diameter of 19mm and a gauge length of 76mm was subjected to tension, with the results shown in Table. Using a computer spreadsheet program, plot the stress–strain relationship. From the graph, determine the Young’s modulus of the steel alloy and the deformation corresponding to a 37kN load.
Q1: The beam shown in Figure 1 is subjected to a vertical force Pv and a horizontal force Ph. The data for Pv, Ph, a,L,and e are shown in Table 1. Determine the maximum compressive and tensile stresses under the vertical force (at a distance a from the left support.) Pv = 80k N a = G0o 6 omm e %3D 26 K N 120 mm L =3600 mm Figure 1 250 mm
Give me right solution
650 600 550 500 450 400 350 300 250 200 150 100 50 0.002 0.004 0.006 0.008 0.01 0.012 0.014 0.016 0.018 0.02 Strain mm/mm The graph above shows the stress-strain relationship of a steel bar under tension test. The steel bar diameter = 8 mm and the bar gauge length = 100 mm. Determine the following: Toughness of the specimen Stress (MPa)
A thin rectangular plate ABCD is deformed into a parallelogram as shown in the figure below. The width of the plate is w = 1300 mm, and the height of the plate is h = 1700 mm. The shear strain at A is known to be +4172 μrad. Assume a = 2.9 mm. Calculate the magnitude of dimension b in the figure.
A cylinder is made of steel plate is intended to be used as a container for compressed air. The dimensions of the cylinder are L=2m, D=60cm, and t = 0.005m. If the ultimate tensile stress of the steel is 400 N/mm², Young's modulus is 200000 MPa and Poisson's ratio is 0.25. 1- Determine the maximum air pressure that can be stored in the cylinder (use factor of safety = 2) 2- Determine the change in the volume of the cylinder due to storing maximum pressure.
The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ε1 = 60 x 10-6, and ε2 = 210 x 10-6. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. E(al)= 10(10^3)ksi V(al)= 0.33
I need the answer as soon as possible
Data taken from a stress-strain test for a brittle alloy are given in the table. The curve is linear between the origin and the first point. o (ksi) e (in./in.) 0 0 44.8 0.0008 54.0 0.0013 57.5 0.0017 59.5 0.0021 60.0 0.0023 Part A Determine approximately the modulus of toughness. The rupture stress is o, 30.0 ksi. Express your answer in inch-pounds per cubic inch as an integer. VAE Ivec U Submit Provide Feedback Request Answer in-lb/in³
Answer in two decimal places please
COMPLETE SOLUTIONS PLEASE WITH FBD
A brass alloy rod having a cross sectional area of 0.24 in.2and a modulus of 16 * 106 psi is subjected to a tensile load. Plastic deformation was observed to begin at a load of 8,944 lb.a. Determine the maximum stress that can be applied without plastic deformation.b. If the maximum length to which a specimen may be stretched without causing plastic deformation is 3.28 in., what is the original specimen length?