For the beam shown on the previous question, determine the values and location of the maximum compressive bending stress and the maximum shear stress if the cross section of the beam is as shown below. (All dimensions are in mm). 300 70 35 550
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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.QUESTION: The distributed load on the T-section beam shown below and moment affects. A is the fixed joint and B is the sliding joint. This beam is made of a ductile material with a yield stress (σak) of 1000 MPa. The thickness (depth) of the beam profile is t=6 mm. A) As a mechanical engineer, check the strength of this beam (in terms of Normal and Shear Stress) ? B) In order for the existing beam to run smoothly, two 100x25 mm plates made of the same material are planned to be welded to this beam. The mechanical engineer working in the factory told the welder to weld this piece under the beam (where the B point is). But the welder, regardless of what the mechanical engineer said, welded this plate to both sides of the existing T-section beam as shown below, thinking that it wouldn't matter anyway. As a mechanical engineer : 1) After welding these plates on both sides of the beam, as the welder did, find out whether the new beam will work smoothly or not by making the necessary…12) For the given curved beam (as shown) with a rectangular cross section, calculate the distance of the neutral axis from the center of curvature. Express your answer in mm, up to 1 decimal place. 13) The bending moment acting on the curved beam with a rectangular cross section is 25 kN-m. What is the bending stress at point B? (Answer must be in MPa, up to 1 decimal place. Add a minus sign if the answer is a compressive stress.)
- A beam having a tee-shaped cross section is subjected to equal 18 kN-m bending moments, as shown. Assume bf = 125 mm, tf = 25 mm, d = 185 mm, tw = 20 mm. Find the following: A. The cross-sectional dimensions of the beam are also shown. B. determine the maximum bending stress (positive if tensile and negative if compressive) produced in the cross section. Express your answer in MPa rounded to the nearest tenths. C. determine the bending stress at point H (positive if tensile and negative if compressive). Express your answer in MPa rounded to the nearest hundredths. D. determine the controlling section modulus about the z axis. Express your answer in (103) mm3 rounded to three significant figures. E. determine the moment of inertia about the z axis. Express your answer in (106) mm4 rounded to three significant figures.Please answer this question, An aluminum rod is rigidly attached between a steel rod and a bronze rod as shown in the figure. Axial loads are applied at the positions indicated. Find the stress of each rod in MPa3. Two plates are connected by bolts as shown in the figure. Compute the maximum axial stress that each plate will handle. The allowable shear stress of each bolt is 50MPa and the diameter of each bolt is 20 mm
- THE BEAMS SHOWN IN FIGURES (a) AND (b) HAS THE FOLLOWING PROPERTIES. f’c =30 MPa, fy=400 MPa AND IS SUBJECTED TO A POSITIVE BENDING MOMENT Mu=140KN-m. ANSWER THE FOLLOWING.1. DRAW THE INTERNAL STRESS AND STRAIN DIAGRAM OF BEAM CONSIDERING THAT THE DEPTH OF THE STRESS BLOCK IS GREATER THAN THE THICKNESS OF THE FLANGE.Consider the nonprismatic cantilever beam of circular cross section shown. The beam has an internal cylindrical hole in segment 1; the bar is solid (radius r ) in segment 2. The beam is loaded by a downward traingular load with maximum intensity q0 as shown. (a) Find expression for maximum compressive stress at point 1. (b) Find expression for maximum tensile stress at point 1.Given a rectangular hollow box with outer dimensions 125mm x 85mm and constant thickness of 10mm has an ultimate stress of 415 MPa. Modulus of Elasticity of 110 GPa. a. Determine the bending moment M for which the factor of safety will be 2.50. b. Determine the corresponding radius of curvature of the section.
- Calculate the bending stress and shear stress values and draw the stress diagrams next to the section. T=10tons,M=-14tm,b=45mm,h=880mm,t=60mm(a) Calculate the maximum tensile bending stress (Express the stress in Pa or MPa) and determine its location with respect to neutral axis. (b) How far is the maximum tensile bending stress located from support A? (Consider x=0 at support A ) (c) Calculate the maximum compressive bending stress (Express the stress in Pa or MPa) and determine its location with respect to neutral axis. Please do question yourself, I've already had this question solved twice but both came up with diffrent results.A beam having a tee-shaped cross section is subjected to equal 18 kN-m bending moments, as shown. Assume bf = 125 mm, tf = 25 mm, d = 185 mm, tw = 20 mm. The cross-sectional dimensions of the beam are also shown. Answer the Following: A. Determine the centroid location (measured upward from the bottom), in mm rounded to the nearest tenths. B. determine the maximum bending stress (positive if tensile and negative if compressive) produced in the cross section. Express your answer in MPa rounded to the nearest tenths. C. determine the bending stress at point H (positive if tensile and negative if compressive). Express your answer in MPa rounded to the nearest hundredths. D. determine the controlling section modulus about the z axis. Express your answer in (103) mm3 rounded to three significant figures. E. determine the moment of inertia about the z axis. Express your answer in (106) mm4 rounded to three significant figures.