Math Problem Statement

As shown, a truss is loaded by the forces P1 = 947 N and P2 = 435 N and has the dimension a = 3.70 m. Determine FBC, the magnitude of the force in member BC, using the method of sections. Assume for your calculations that each member is in tension, and include in your response the sign of each force that you obtain by applying this assumption.

As shown, a truss is loaded by the forces P1 = 947 N and P2 = 435 N and has the dimension a = 3.70 m. Determine FBC, the magnitude of the force in member BC, using the method of sections. Assume for your calculations that each member is in tension, and include in your response the sign of each force that you obtain by applying this assumption.

Solution

To solve for the force in member BCBC (denoted as FBCF_{BC}) using the method of sections, we need to follow these steps:

1. Analyze the Truss Structure and Section

The truss is symmetric, and we will use a vertical section that cuts through members BCBC, GCGC, and CHCH. This will allow us to isolate one side of the truss for easier analysis.

2. Free-Body Diagram

We will draw a free-body diagram of either the left or the right portion of the truss (after cutting through the truss). For simplicity, let’s cut the truss through members BCBC, GCGC, and CHCH, and consider the left part of the truss (from AA to GG).

3. Calculate Reaction Forces

We need to calculate the reactions at supports AA and EE.

  • AA is a pinned support, so it has both horizontal (AxA_x) and vertical (AyA_y) reactions.
  • EE is a roller support, so it only has a vertical reaction (EyE_y).

Using equilibrium equations for the entire truss:

  • Sum of forces in the xx-direction: Fx=0    Ax=0\sum F_x = 0 \implies A_x = 0 (no horizontal forces are applied).

  • Sum of forces in the yy-direction: Fy=0    Ay+Ey=P1+P2\sum F_y = 0 \implies A_y + E_y = P_1 + P_2 Substituting P1=947NP_1 = 947 \, \text{N} and P2=435NP_2 = 435 \, \text{N}, we get: Ay+Ey=947+435=1382NA_y + E_y = 947 + 435 = 1382 \, \text{N}

  • Moment about point AA (taking counterclockwise moments as positive): MA=0    Ey3aP2(2a)P1a=0\sum M_A = 0 \implies E_y \cdot 3a - P_2 \cdot (2a) - P_1 \cdot a = 0 Substituting P1=947NP_1 = 947 \, \text{N}, P2=435NP_2 = 435 \, \text{N}, and a=3.7ma = 3.7 \, \text{m}: Ey(3×3.7)435(2×3.7)9473.7=0E_y \cdot (3 \times 3.7) - 435 \cdot (2 \times 3.7) - 947 \cdot 3.7 = 0 Simplifying: Ey11.13222.93503.9=0E_y \cdot 11.1 - 3222.9 - 3503.9 = 0 Ey11.1=6726.8E_y \cdot 11.1 = 6726.8 Ey=6726.811.1=606NE_y = \frac{6726.8}{11.1} = 606 \, \text{N}

  • From Ay+Ey=1382NA_y + E_y = 1382 \, \text{N}, we find: Ay=1382606=776NA_y = 1382 - 606 = 776 \, \text{N}

4. Analyze the Section

Now, let's apply the method of sections. We will analyze the left part of the truss and apply the equilibrium equations.

  • Sum of forces in the yy-direction: Fy=0    AyP1FBCsin(θ)=0\sum F_y = 0 \implies A_y - P_1 - F_{BC} \cdot \sin(\theta) = 0 where θ\theta is the angle of member BCBC with the horizontal.

  • Sum of moments about point GG (to eliminate forces in members GCGC and CHCH): MG=0    AyaFBCa=0\sum M_G = 0 \implies A_y \cdot a - F_{BC} \cdot a = 0 Solving for FBCF_{BC}, we get: FBC=Ay=776NF_{BC} = A_y = 776 \, \text{N}

Thus, the magnitude of the force in member BCBC is FBC=776NF_{BC} = 776 \, \text{N}.

Conclusion:

The force in member BCBC is 776N776 \, \text{N}. Since we assumed all members to be in tension, the positive sign confirms that the force is tensile.


Would you like further details on any step, or to ask about another topic?

Here are 5 related questions you might be interested in:

  1. How would the analysis change if the load P2P_2 was increased?
  2. What if we analyzed the right section of the truss instead?
  3. How do we determine if a member is in tension or compression?
  4. How is the method of joints different from the method of sections?
  5. Can this method be applied to trusses with inclined supports?

Tip: When calculating moments, choose points where multiple unknown forces act to simplify the equations.

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Math Problem Analysis

Mathematical Concepts

Static Equilibrium
Truss Analysis
Method of Sections

Formulas

Sum of Forces (ΣF = 0)
Sum of Moments (ΣM = 0)
Component Force Calculations

Theorems

Static Equilibrium in Two Dimensions

Suitable Grade Level

University Level - Engineering