find the temperature distribution of the beam shown below, takke of=0.1 C loko I, and L-1m- Co -10 C° 30 со 9-30tw R = lokw/m²/" 16215° he 5Kwlm² ke T = 250°
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I need answer with diagram and not from AI
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shown below, takke of=0.1
C
loko
I, and L-1m-
Co
-10 C°
30 со
9-30tw
R = lokw/m²/"
16215°
he 5Kwlm² ke
T = 250°"
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Step by step
Solved in 2 steps with 1 images
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- W A Strain gage W NA A L b Side view Lo Front view A cantilever beam has the following parameters: Lo - 0.24 m L-0.17 m b- 0.028 m h- 3.16 mm Yield stress -349.64 MPa Calculate the largest load W that can be applied before the beam yields.Consider the material Al-$456 It has the following physical ploperties Syleld = 230mPA %3D s-72GPA (modulos elasticity) Oultimate=315 mPA G- 28GPA Cmad vlus rigidity) Tuield =130 mPA Joltimate=185 mPA A Calculate Poisson's ratio B) If we have a following dimensions And Forces 3-0 block of Al-5456 with the Ex =800N X= Bcm Fy=1000N ) Is Our block Safes (consider only plane stes) Dset up the 3 eqetions to find the strains (Ex Ey E2) in each directian E Solve the 3exuations to find the Einal dimensions of our blockA steel I-beam to is designed under the tank for holding it. You know that the deflection of the beam should be limited in order to provide stability for the structure, Therefore, you start with calculating the deflection of the beam under the weight of the tank that can be assumed as a distributed load as shown below. Giver 0.76 in 0.1 k/in A L = 108 in OB 14.92 in N.A. 0.543 in E = 29000 ksi 10.47 in 28.32 in 0.76 in Find: (a) Using equilibrium, solve for the reactions for the beam. (b) Draw the V, M diagram for the beam shown. Label all key points. (c) Calculate the value of the moment of inertia about the neutral axis. (d) Using the method of integration, calculate the equation of the deflected shape of the beam, y(x). (e) Calculate the maximum deflection of the beam under the weight of the tank.
- Beam loaded as shown in Fig. P-404. 2000 lb M = 4800 lb-ft D 3 ft RA 6 ft 3 ft Ro Figure P-404Please give the solution clearly, I will vote it up for your effort thank you in advance. LOVE YOU :)Sy Math Solver Consider the wing channel in (Figure 1) with h = 3.4 in. Neglect the effect of rounded corners. The material has a uniform thickness of 0.5 in. <1 of 1 Figure J 3 in. E 2 in. 2 in. 3 in.. SA Cup Document.. ✔ STATICS HW C Part A:Determine... Mom Insurance Part A Determine which locates the centroid of the cross-sectional area of the wing channel. Express your answer in inches to three significant figures. VO 16 It ? in. Request Answer Part B Determine the moment of inertia I about the centroidal z' axis. Express your answer in inches to the fourth power to three significant figures. ? [ΨΕΙ ΑΣΦ | VE IN in4 Iz Submit Submit Request Answer Pearson 2 Dravida 5andhaak
- hi can use please answer question for attached A uniform plank has length 6m and mam 40kg It is placed on horizontal ground at the edge of a vertical river bank, so that 1.5m of the plank is peojecting over the edge, as shown in Figure.27. if you use * can you please tell me what u mean by it?A steel bar 2m long, 20 mm wide and 10 mm thick is subjected to a pull of 20 kN inthe direction of its length. Find the change in thickness. Take E-200 GPa and Poisson'sRatio 0.30how to get the -y theo
- W A L A Test beam Strain gauge (a) Unsymmetrical cantilever beam with weight applied at the free end and at the "shear centre", so that there is no torsion induced. Section A-A Strain gauge 1 b Strain gauge 3 Strain gauge 2 B (b) Location of Huggenberger strain gauges a Referring to the above figure, calculate the location of the centroid, the second moments and product of area for the cross-section if; D = 67 mm B = 41 mm t = 2.41 mm. From these, calculate the position and orientation of neutral axis for pure bending in the vertical plane (i.e. bending about a horizontal axis). Also calculate the directions of the principal second moments of area. Next, graph as scale diagram of the cross-section and plot the neutral axis on that diagram in the correct location and indicate the direction of deflection for the same conditionsHello I am try to solve this loads and reactive forces problem 1.7 problem as I am having difficult time understanding how the distributed load is 7 ft. Where did the 7ft come from and why is it 7ft and and not 3ft? what am I doing wrong? How I got 3 ft . I added 3+3 = 6ft which means that the distributed load is 3ft500mis wooden b1ock so mis 30° bollet travelling So0 mis at 3 kg hits the blocu. It 'exi's the Othe Side. at. 50 mis. • Deteimine t (Hime) 1+ '+alkes for. the biocu Stop. Sliding
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