Determine the maximum bending stress acting at the cross-section a-a. The cross-section is solid circular with a diameter of 100 mm. Take the moment of inertia about the NA, 1 = 4.909 x 10-6 m4. a 30 kN 0.5 m 0.5 m Select one: 597 MPa 102 MPa 250 MPa 398 MPa 199 MPa 2 m D = 100 mm Time left 0:26:38
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- The true optionBelow 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. 125mmDetermine the bending stress at point B and C
- Below Figure shows the section of an angle purlin. A bending moment of 60 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 BỊ 10mm 30° C ID 10mm 57 MPa. 89 MPa. Non Above 72 MPa. 125mmof on If the I-flange beam is subjected to a shear force V= 20 kN, calculate the transverse shear stress at the point A (considered located on the web part). The area moment of inertia of that section about its neutral axis N.A. is INA = 44.167 x (10) m². Flange Web. Select one: O 10 Mpa O 4.95 MPa O 41 MPa O 100 MPa O50 MPa 20 mm 100 mm A 100 mm 25 mm 150 mm 25 mm Time left 0:46:01 sDetermine the internal forces (axial force, shear force, and bending moment) at point j of the indicated structure, teta = 0 º
- If the beam is subjected to an internal moment of M = 100 kN*m, determine the bending stress developed at points A, B, and C. Sketch the bending stress distribution on the cross section. Construct the stress distribution in 2D similar to in-class examples, rather than isometrically similar to the textbook examples for clarity. 30 mm A B 300 mm M 150 mm 150 mm 30 mmDetermine the ff: •Internal bending moment at point c •internal shear force at point c •internal normal force at point c Asap please.Determine the torsional shear stress in the shaft section AB and BC. There is a fixed support at C that can resist a moment. (Image taken from Statics and Mechanics of Materials by Beer, Johnson, DeWolf and Mazurek) T₁ = 300 N-m 30 mm TB = 400 N-m 46 mm 055 Shear Stress in AB = Shear Stress in BC= B 0.9 m 0.75 m units: units:
- The simply supported beam is subjected to the force F-600 N and the uniform distributed load with intensity w=450 N/m. Draw the shear force and bending moment diagrams (in your homework documentation) and determine the equations for V(z) and M(2). Take 2 = 0 at point A. 19 W B F 2013 Michael Swanbom BY NC SA D Χ a. -b- - Values for dimensions on the figure are given in the following table. Note the figure may not be to scale. Variable Value α 4 m b 2 m с 3 m Determine the maximum shear force (magnitude) and its location in the beam, and the maximum bending moment (magnitude) and its location in the beam. Note: On an exam, you may be required to actually sketch the shear and moment diagrams, but there is no reasonable way to assess this on WAMAP. Maximum shear stress: Vmax Maximum bending moment: Max = N located at x = m Nm located at x = mS = 70The aluminium machine part shown below is subjected to a moment of M = 75 N.m. Determine the bending stress created at points B and A on the cross section. Sketch the results on a volume element located at each of these points. A- 50mm 50mm 100mm 100mm 20mm B- M=8kN-m 20mm