F 2 ft 2 ft 2 ft- 2 ft 1.5 ft - 40 Ib 60 lb 80 Ib 80 Ib

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Chapter1: Units, Trigonometry. And Vectors
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Answer the following question: 1. The internal drag truss for the wing of a light airplane is subjected to the forces shown. Using the method of joints, determine the forces in all of the members and state if the members are in tension or compression. (Include free body diagram)
The image depicts a truss structure within a beam subjected to multiple loads and displays the following details:

- **Structure Layout:**
  - The beam is divided into sections by vertical lines labeled A through E on the bottom and J through F at the top.
  - Distances along the beam are marked, illustrating segments of 2 feet and 1.5 feet. 
  - Three sections each span 2 feet (from A to B, B to C, and C to D), while the section from D to E is 1.5 feet long.

- **Forces:**
  - Four downward forces are applied at points B, C, D, and E.
  - At points B and C, there are forces of 80 lb each.
  - At point D, there is a force of 60 lb.
  - At point E, a force of 40 lb is applied.

- **Truss Configuration:**
  - The trusses are arranged with diagonal members connecting the top and bottom points (A to I, I to H, H to G, G to F, J to B, I to C, and H to D).
  - The top points (J, I, H, G, F) and bottom points (A, B, C, D, E) are set 2 feet apart vertically.

This setup is often used in structural engineering to analyze the distribution of forces and stresses in beams and trusses.
Transcribed Image Text:The image depicts a truss structure within a beam subjected to multiple loads and displays the following details: - **Structure Layout:** - The beam is divided into sections by vertical lines labeled A through E on the bottom and J through F at the top. - Distances along the beam are marked, illustrating segments of 2 feet and 1.5 feet. - Three sections each span 2 feet (from A to B, B to C, and C to D), while the section from D to E is 1.5 feet long. - **Forces:** - Four downward forces are applied at points B, C, D, and E. - At points B and C, there are forces of 80 lb each. - At point D, there is a force of 60 lb. - At point E, a force of 40 lb is applied. - **Truss Configuration:** - The trusses are arranged with diagonal members connecting the top and bottom points (A to I, I to H, H to G, G to F, J to B, I to C, and H to D). - The top points (J, I, H, G, F) and bottom points (A, B, C, D, E) are set 2 feet apart vertically. This setup is often used in structural engineering to analyze the distribution of forces and stresses in beams and trusses.
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