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Answer #1 and use AREA METHOD only.
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- A circular pipe of internal diameter 30 mm and thickness 4 mm is subjected to a force 30 kN and the elongation was measured as 1 mm. If the length of the pipe is 2 m, find the value of Young's modulus of elasticity and the stress in the pipe. Match each item to a choice: Young's Modulus (GPa) Stress (MPa): Choices: : 140.4 # 47.9 B 56.4 # 120.8 #240.8 8 70.27.5 x104 Problene # 3: if whether lach reod component a)ldentify ene w under compression or tension. り Solve for area n rod given square each cross se etions Catuen valnes: Stress in each nod: Steed: 7.5 xl04 KN /m? bronde: 1.0 a10 s kN Imr aluminum: lis K105 KN /m? lkN 4KN 3KN テ ムN- stael Gonze alu minim3) Solve the plane stress problem using two-element model to find displacements and stresses. 15 kN 30 mm E-70 GPa Thickness - 10 mm
- FThe Airy stress function for a cantilever beam loaded by a force applied at the opposite side to the built-in end is given by p=Axy 3 where the x coordinate runs along the length of the beam, the y coordinate runs along the width of the beam and A is an arbitrary constant which can be determined through application of boundary conditions. Which equation gives the shear stresses, ? O 0 O 6Axy O-3Ay² O-6Axy(3) A slencer rod is Subgected to tenstan, the lood is inceeased incrementally (MP) = 160 * 10 320M Pa and the plot at left'is obtined. 320 * What can be said for ultimate stronpth? 0.004 0.002 *The wateriel which the rod is node of, duc tile noteriel, *If the loading is kept until to J iš 320MPA withdrawn auddnly ond is a explain why? what will Be ethe permanant stroin? the looding is ceosed at some lovel and the rod is released and Eenp lengineering strain) Come out t be 0,003, what will bĕ the Correspendany true stran CE)?
- 11:11 A The wood beam has an allowable shear stress of Tallow = 9.6 MPa. d3 d3 Variable d₁ d₂ d1 d3 d4 d5 wamap.org Value d2 V Values for the figure are given in the following table. Note the figure may not be to scale. 0.05 m 0.125 m 0.05 m 0.225 m P 0.1125 m d1 d5 a. Determine the Q at point P. b. Determine the moment of inertia, I. d4 c. Determine the magnitude of the max shear force that can be applied to the cross-section at point P, Vmax.stress 0.02 0.018 0.016 0.014 0.012 0.01 0.008 0.006 0.004 0.002 0.05 0.1 0.15 0.2 0.25 0.3 0.35 Determine : 1- Stress, Stratn care 2. elastic Zone 3. yield sbresscoys 4- plastic Zone 5- UItimate Stress Cous 6- Elongation 7- propotionaL stress cops 8-fructurc stress coF)The internal loadings at a section of the beam in (Eigure 1) are shown Figure 20 mm 100 mm 200 mm 20 mm 10 kNm 20 mm 10/12 60 kN 80 KN 500 N-m Determine the in-plane principal stresses at point C. Also compute the maximum in-plane shear stress at this point Express your answers, separated by commas, to three significant figures. VAZ Ivec 4 d Submit Provide Feedback T Wha Bequest Answer ? MPA, MPA, MPA
- Solve the alternating force, Fmax, Fmin, alternating stress, midrange stress, max stress, min stress sing the Modified Goodman equation for a factor of safety of 1..2-8 The stress-strain data from a tensile test on a cast-iron specimen are Engineering stress, MPa 35 70 112 133 182 224 280 332 343 378 5.0 Engineering strain, e • 10 mm/mm 0.20 0.44 0.80 1.0 1.5 2.0 2.8 3.4 4.0 Plot the stress-strain locus and find the 0.1 percent offset yield strength, and the tangent mod- ulus of elasticity at zero stress and at 140 MPa.I. A steel rod is acted upon by the loading shown below. 50 mm² is the area of the circular rod. The coupling sizes at B, C, and D are neglected. Use E st = 200 GPa -1 m 1.5 m- -1.25 m A 9 kN B C 4 kN D 2 kN Solve for the following: kN , (insert type of force here) kN, (insert type of force here) kN, (insert type of force here) Force in segment AB, PAB Force in segment BC, PBC Force in segment CD, PCD Total deformation in the assembly, & = mm II ||