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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- problem 1.3-9 solution plz....1. A tripod shawn supports of note that ball and rocket joints are used to mount the tripuod a load P=1000N at point A. Take at points B,D, and C. consider the t LI L 2 L2: 4 L3 : 3 A : 45° g :30° %3D on x-z plane L2 POINT C (2,-2,3) C0,0,0) ミー- Determine the ff Force of AB - N Force of AC - N Force of AD : NW 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.
- A beam in Fig. 3a and Fig. 3b is supported by a roller at A and a pin at C. Determine the horizontal and vertical components of support reactions on the beam if a = 3 m and L = 9 m for conditions in Fig. 3a and Fig. 3b, respectively.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 block05) Find the minimum volume of the truss shown with constraints on the depth of the truss (y), cross-sectional areas of the bars (Al and A2), and the stresses induced in the bars (ol and o2). Treat y, Al, and A2 as design variables with oi < 105 Pa (i 1, 2), 1 msys4 m, and 0< Ai <0.2 m2 (i = 1, 2). 9 m y Bar I Bar 2 (area = Ap) (arca = A3) P = 1000 N
- Please answer what is being asked and show full solutions with necessary diagrams. "Strength of Materials" ProblemConsidering the effects of the prestressing forces (assume no loss) and the working loads (include the selfweight of the beam). Calculate the stress indicated below. Calculate fbot at midspan. (MPa), consider sign convention (- for compression, + for tension) Ex CLUD In6 SELFWEI6HT 300 = P P= 300 kN I5M 400 de = 24 1N m3 N.A. 800 70Problem 7: Non-circular cross section shaft related to torque problems are difficult to be solved using the basic theory as for circular shaft. Your role is to make use of FAE to analyze the stress in squared cross section shaft shown in Figure.5. g= 6.5(10%) N/cm? e = 0.035 deg 0.5 cm 0.5 cm 0.5 cm- 0.5 cm Figure.5: Squared cross section shaft applied to torque T as 3D model Provide justified explanation and recommendations to simplify the problem from three-dimensional (3D) to two- dimensional (2D). b. а. If the governing boundary value problem equation of such a problem can be given by: + 2g0 = 0, dy? $(x,y) at boundary is 0 dx2