- ahmad alhayek




Problem


The boom of a crane has a rectangular box section with the dimensions shown. Determine the principal stresses in the boom at points A and B. Neglect the weight of the boom, 

pulley, and cable.



Step-by-step solution

  1. Step 1 of 12

    Draw the free body diagram of the beam as follow:
    Picture 39



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  2. Step 2 of 12

    Apply force equilibrium condition along axial direction.



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  3. Step 3 of 12

    Apply force equilibrium condition along vertical direction.



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  4. Step 4 of 12

    Apply moment equilibrium condition about node A.



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  5. Step 5 of 12

    Apply the equation for moment of inertia, , for a hollow rectangle.
    Here, the width of the outer rectangle is, the height of the outer rectangle is, the width of the inner rectangle is, and the height of the inner rectangle is,
    Substitute 100 mm for, 150 mm for, 90 mm for, and 140 mm for .



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  6. Step 6 of 12

    Apply the equation for area, , of the rectangle.
    Substitute 100 mm for, 150 mm for, 90 mm for, and 140 mm for .



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  7. Step 7 of 12

    Apply the formula for static moment of area, , at point .
    Substitute  forfor, for, and  for.
    Apply the formula for shear stress at point A.
    Substitute for for for , 90 mm for , and 100 mm for .



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  8. Step 8 of 12

    Apply the formula for the normal stress at point A.
    Substitute  for and  for.



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  9. Step 9 of 12

    Apply the formula for the average normal stress at point A.
    Substitute  for.



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  10. Step 10 of 12

    Apply the formula for the radius of Mohr’s Circle for point A.
    Substitute  for  and  for.



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  11. Step 11 of 12

    Apply the formula for the principle stresses at point A.
    .
    Substitute  for  and  for to calculate the maximum and the minimum principal stresses at point.
    Therefore, the stresses at point are and.



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  12. Step 12 of 12

    Apply the formula stresses at point B by using Equation 9.10.
    Substitutefor, for for  for  and  for .
    Point lines on the bottom surface of the boom, so there is no shear stress.
    Thus, the stresses at point  are and.



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ahmad alhayek تصميم ahmad alhayek جميع الحقوق محفوظة 2016

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