Determine the internal resisting forces and moment trans- mitted by section aa in 500 Ib 10 in- -5 in- 45 B 7 in. 8 in.
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- Below Figure shows the section of an angle purlin. A bending moment of 5 kN.m is applied to the purlin in a plane at an angle of 30 deg to the vertical y axis. If the sense of the bending moment is such that both its components Mx and My produce tension in the positive xy quadrant, calculate the maximum direct stress in the purlin, stating clearly the point at which it acts. * 100 mm E 10mm 30 C D -10mm 57 MPa. 89 MPa. Non Above O 72 MPa. 125mmThe 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-7Solve Problem 11.3-3 for a W 10 × 45 steel column having a length L = 28 ft.
- Determine the bending moment M in the pinned-end column with eccentric axial loads shown in the figure. Then plot the bending-moment diagram for an axial load P = 0.3Pcr. Note: Express the moment as a function of the distance x from the end of the column, and plot the diagram in nondimensional form with M/Pe as ordinate and x/L as abscissa.A square tube section has side dimension of 20 in. arid thickness of 0.5 in. If the section is used for a 10-ft-long beam subjected to 1250 kip-in, torque at both ends, calculate the maximum shear stress and the angle of twist between the ends. Use G = 11,600 ksi.A steel W 310 x 52 column is pin-supported at the ends and has a length L = 4 m. The column supports two eccentrically applied loads J\ = 750 kN and P2= 500 kN (see figure). Bending occurs about axis 1-1 of the cross section, and the eccentric loads are applied on axis 2-2 at distances of 200 mm from ccntroid C. Calculate the maximum compressive stress in the column. Assume that modulus elasticity E = 200 GPa.
- Repeat Problem 6.2-1 but now assume that the steel plate is smaller (0.5 in. × 5 in.) and is aligned with the top of the beam as shown in the figure.plz help before -ront The shaft is supported at its ends by two bearings A and B and is subjected to the forces applied to the pulleys fixed to the shaft. (Figure 1) The T₁ 410-N forces act in the - direction and the 200-N and 80-N forces act in the +y direction. The journal bearings at A and B exert only y and components of force on the shaft. Figure lashel but sol is 300 mm A 200 mm 2 150 mm 150 mm ✓ 200 mm 400 mm B. 200 N 200 N 80 N 80 N 1 of 1 ▾ Part B Determine the resultant shear force in the y direction on the cross section at C Express your answer to three significant figures and include appropriate units. (Vc)y=245.714 Submit Part C Submit * Incorrect; Try Again; 3 attempts remaining Check your signs. (Vc),= 175 ▾ Part D Determine the resultant shear force in the direction on the cross section at C. Express your answer to three significant figures and include appropriate unite. T= 10 ▾ Part E Previous Answere (Mc) Submit M ^ Part Fi * Incorrect; Try Again; 5 attempts remaining…with the following modifications: Add an additional force P = 20kN acting downwards at point B
- A 15' 10' 10 kips 10' C E 10 kips 10' Determine the internal force on: Member EF positive (+) if Tension and negative (-) if Compression 20' F 10 kips 10' 10 kips 10' 15' 10' 10 kips BSolve For the sum of moment oF all Forces dockwise direction is pasitive at point A, B, I D. Include all moments. 2m ES J0ON A 100 N-m G=8ON 2m 2m 55N.m R= 90N 2m 2m P= 120N 2m 2m 2m 2mAssume the following : -b- wb W = 100N/m; a = 5m; b = 8m; c = 6m %3D (1-5)Max. Moment occurs @ x = _(fr R1) R, R2 (6-10) Max. moment = N-m