Find the transverse shear stress in the material 3 in. from the top surface of the beam shown in the following figure.
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- The Z-section of Example D-7 is subjected to M = 5 kN · m, as shown. Determine the orientation of the neutral axis and calculate the maximum tensile stress c1and maximum compressive stress ocin the beam. Use the following numerical data: height; = 200 mm, width ft = 90 mm, constant thickness a = 15 mm, and B = 19.2e. Use = 32.6 × 106 mm4 and I2= 2.4 × 10e mm4 from Example D-7A cross section in the shape of a circular arc of constant thickness is shown in the figure. Derive the following formula for the distance e from the center of the arc to the shear center S: in which ß is in radians. Also, plot a graph showing how the distance e varies as ß varies from 0 to tlThe cross section of a sign post of constant thickness is shown in the figure. Derive the formula for the distance e from the cent crime of the wall of the post to the shear center S: where I2. = moment of inertia about the z axis. Also, compare this formula with that given in Problem 6.9-11 for the special case of ß = 0 here and a = h/2 in both formulas.
- Determine the shape factor f for a cross section in the shape of a double trapezoid having the dimensions shown in the figure. Also, check your result for the special cases of a rhombus (b1= 0) and a rectangle (b1= b2).The cross section of a steel beam is shown in the figure. This beam is subjected to a bending moment M having its vector at an angle 8 to the - axis. Determine the orientation of the neutral axis and calculate the maximum tensile stress tiand maximum compressive stress tcin the beam. Assume that e = 22.5° and M = 4.5 kN · m. Use cross-sectional properties Ix=93.14 × 106 mm4, Iy= 152.7 X 10e mm4, and 9 = 27.3º.Derive the following formula for the distance e from the centerline of the wall to the shear center S for the hat section of constant thickness shown in the figure: Also, check the formula for the special case of a channel section (a = 0).
- (14) Find the total shear load on each of the three bolts for the connection shown in the figure and compute the significant bolt shear stress and bearing stress. Find the second moment of area of the 8-mm plate on a section through the three bolt holes, and find the maximum bending stress in the plate. (Ans/1.48(10 mm4, 110 MPa) Holes for M12 x 1.75 bolts 8 mm thick 36 12 KN 32 Dimensions in 64 millimeters 36 200- ColumnQ1/ A composite beam is made of wood and reinforced with steel strap located on its bottom side. It has the cross-sectional area shown in fig. if the beam is subjected to a bending moment of M=2kN.m, determine the normal stress at wood and steel. Take Ew=12Gpa and Est=200Gpa. 150mm Wood en 20mm Steel 150mmThe beam shown in the figure is made of Wood that has an Allowable Shear Stress of 200 psi; Determine the maximum value of Shear Force "V" that the section could withstand?, also draw the distribution of the shear stress over the section of the beam 12 in. 8 in.
- Find the maximum shear force (V), the cross section can carry if the maximum shear stress is not to exceed 100MPa. And then after calculating the value of V, FIND the force carried by the web. 200 mm 20mm 20mm V 210mm 20mm 110mmFor the beam shown at right, determine the following: P= 1800 lb a. Maximum tensile bending stress b. Transverse shear stress at a the junction of the "TEE" (i.e., 2" above the neutral axis). c. Transverse shear stress at the neutral axis - 7.5 ft- - 7.5 ft- (a) d. Draw the stress elements -10 in. representing the state of stress at the junction of the “TEE" and at the neutral axis. | 2 in. 4 in. -N- 1600 10 in. 8 in. 42 in.k- (b)Q2 The internal bending moment in a beam with a cross sectional area shown in the figure is 500a in the direction shown. Nom Find: a) The centroid of the cross sectional area and, b) the maximum tensile and compressive normal stresses. Make a sketch showing the stress distribution A A -35 mm C2 100 mm C1 = ỹ 5 G0 Na m 25 mm B 50 25 50. mm 'mr mm