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wonghuien's Question
Physics M
Posted 4 months ago
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Question 5
For the beam shown below;
a) Calculate the support reactions.
Ans: Ay=127.5 kN, By =212.5kN=212.5 \mathrm{kN}
b) Draw a free body diagram (FBD) of the left section of the beam, with the cut made 4.5 m to the right of support A. Using your FBD and applying the equilibrium equations ΣFy=0\Sigma \mathrm{F}_{\mathrm{y}}=0 and ΣMz=0\Sigma \mathrm{M}_{\mathrm{z}}=0, calculate the value of the shear and the moment at this location.
(For additional practice, in your own time, you can consider an FBD to the right of the cut including support B.)
c) Draw a FBD of the left section of the beam, now cutting through the beam between points AA and BB. In your FBD define the distance between point AA and the cut using the parameter ' xx ', where 0 m<x<8.0 m0 \mathrm{~m}<x<8.0 \mathrm{~m} and x=0x=0 lies at AA. Using your FBD and applying equilibrium equations, derive the general mathematical expressions for the shear force and bending moment in the beam in terms of the parameter ' xx '. Check your answer in part b) by substituting x=4.5 mx=4.5 \mathrm{~m} into your general moment equation.
(For additional practice, in your own time, derive equations where the origin lies at the cantilever tip C. You can check the equivalency of your equations by substituting in numerical values.)
d) Draw the Shear force and Bending moment diagrams and sketch the corresponding deflected shape. It is recommended you draw your SFD and BMD aligned with the beam based on the lines shown below.
(You will not be asked to draw a SFD or BMD in the Content test)
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Answer from Sia
Posted 4 months ago
Solution
a
To calculate the support reactions at points A and B, we first apply the equilibrium equations. The sum of vertical forces must equal zero: ΣFy=0\Sigma F_y = 0. The vertical forces include the reactions at supports A and B, the distributed load, and the concentrated load. The distributed load over the 8 m section is 40kN/m×8m=320kN40 \, \text{kN/m} \times 8 \, \text{m} = 320 \, \text{kN} acting downward, and the concentrated load at C is 20 kN also acting downward. Thus, we have: Ay+By32020=0A_y + B_y - 320 - 20 = 0. This simplifies to Ay+By=340kNA_y + B_y = 340 \, \text{kN}
b
Next, we apply the moment equilibrium about point A to find the reaction at B. The clockwise moment at A is 50 kNm, and the counterclockwise moment due to the distributed load and concentrated load can be calculated as follows: The moment due to the distributed load (acting at its centroid, 4 m from A) is 320kN×4m=1280kNm320 \, \text{kN} \times 4 \, \text{m} = 1280 \, \text{kNm}, and the moment due to the concentrated load at C (3 m from B, or 8 m from A) is 20kN×8m=160kNm20 \, \text{kN} \times 8 \, \text{m} = 160 \, \text{kNm}. The moment equilibrium equation is: 50+By×81280160=0-50 + B_y \times 8 - 1280 - 160 = 0. Solving for ByB_y gives us By=212.5kNB_y = 212.5 \, \text{kN}
c
Now, substituting ByB_y back into the vertical force equilibrium equation gives us: Ay+212.5=340A_y + 212.5 = 340, leading to Ay=127.5kNA_y = 127.5 \, \text{kN}. Thus, the support reactions are confirmed as Ay=127.5kNA_y = 127.5 \, \text{kN} and By=212.5kNB_y = 212.5 \, \text{kN}
d
For the free body diagram (FBD) of the left section of the beam, we cut the beam 4.5 m to the right of support A. The shear force VV at this section can be calculated as: V=Ay(distributed load over 4.5 m)V = A_y - \text{(distributed load over 4.5 m)}. The distributed load over 4.5 m is 40kN/m×4.5m=180kN40 \, \text{kN/m} \times 4.5 \, \text{m} = 180 \, \text{kN}. Therefore, V=127.5180=52.5kNV = 127.5 - 180 = -52.5 \, \text{kN}. The bending moment MM at this section is given by: M=Ay×4.5(moment due to distributed load)M = A_y \times 4.5 - \text{(moment due to distributed load)}. The moment due to the distributed load is 180kN×2.25m=405kNm180 \, \text{kN} \times 2.25 \, \text{m} = 405 \, \text{kNm}. Thus, M=127.5×4.5405=573.75405=168.75kNmM = 127.5 \times 4.5 - 405 = 573.75 - 405 = 168.75 \, \text{kNm}
Answer
A_y = 127.5 kN, B_y = 212.5 kN
Key Concept
Static Equilibrium: The sum of forces and moments acting on a body at rest must be zero. Equations: Fy=0\sum F_y = 0 and M=0\sum M = 0.
Explanation
By applying the equilibrium equations, we can determine the support reactions and analyze the shear and moment at specific points along the beam. This is essential for understanding the internal forces and moments in structural elements.

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