The moment M acting on the cross section of the tee beam is oriented at an angle of 0 = 64° as shown. Dimensions of the cross section are b₁ = 245 mm, t₁ = 22 mm, d = 279 mm, and tw = 18 mm. The allowable bending stress is 205 MPa. What is the largest bending moment M that can be applied as shown to this cross section? 0 D bf y -tw B d
The moment M acting on the cross section of the tee beam is oriented at an angle of 0 = 64° as shown. Dimensions of the cross section are b₁ = 245 mm, t₁ = 22 mm, d = 279 mm, and tw = 18 mm. The allowable bending stress is 205 MPa. What is the largest bending moment M that can be applied as shown to this cross section? 0 D bf y -tw B d
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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![**Educational Website Text Transcription:**
---
**Problem Statement:**
Determine the distance in the y-direction from line DC to the centroid of the area. Then calculate the area moment of inertia about both the x-axis and the y-axis.
**Answer:**
- \( \bar{y} = \) [input box] mm
- \( I_x = \) [input box] mm\(^4\)
- \( I_y = \) [input box] mm\(^4\)
[Button: eTextbook and Media]
[Button: Submit Answer]
---
**Part 2:**
The x-component of moment M will cause compression at A and B, and tension at C and D. The y-component of moment M will cause compression at A and D, and tension at B and C. The maximum tensile bending stress will occur at point C. Calculate the magnitude of the largest bending moment that can be applied so that the stress at corner C does not exceed 205 MPa.
**Answer:**
- \( M = \) [input box] kN⋅m
[Button: eTextbook and Media]
[Button: Submit Answer]
---
**Part 3:**
The x-component of moment M will cause compression at A and B, and tension at C and D. The y-component of moment M will cause compression at A and D, and tension at B and C. The maximum compressive bending stress will occur at point A. Calculate the magnitude of the largest bending moment that can be applied so that the stress at corner A does not exceed 205 MPa.
**Answer:**
- \( M = \) [input box] kN⋅m
[Button: eTextbook and Media]
[Button: Submit Answer]
---
**Part 4:**
Determine the maximum bending moment that can be applied to this cross section.
**Answer:**
- [Input box]
[Button: eTextbook and Media]
[Button: Submit Answer]
---
Note: No specific graphs or diagrams are present in the image to describe further.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F99e37c92-095a-4cae-adf6-01aeaaa5668c%2F5884d7b1-a3f3-44c7-8a81-d6dcf67e925b%2F9xdmjv_processed.png&w=3840&q=75)
Transcribed Image Text:**Educational Website Text Transcription:**
---
**Problem Statement:**
Determine the distance in the y-direction from line DC to the centroid of the area. Then calculate the area moment of inertia about both the x-axis and the y-axis.
**Answer:**
- \( \bar{y} = \) [input box] mm
- \( I_x = \) [input box] mm\(^4\)
- \( I_y = \) [input box] mm\(^4\)
[Button: eTextbook and Media]
[Button: Submit Answer]
---
**Part 2:**
The x-component of moment M will cause compression at A and B, and tension at C and D. The y-component of moment M will cause compression at A and D, and tension at B and C. The maximum tensile bending stress will occur at point C. Calculate the magnitude of the largest bending moment that can be applied so that the stress at corner C does not exceed 205 MPa.
**Answer:**
- \( M = \) [input box] kN⋅m
[Button: eTextbook and Media]
[Button: Submit Answer]
---
**Part 3:**
The x-component of moment M will cause compression at A and B, and tension at C and D. The y-component of moment M will cause compression at A and D, and tension at B and C. The maximum compressive bending stress will occur at point A. Calculate the magnitude of the largest bending moment that can be applied so that the stress at corner A does not exceed 205 MPa.
**Answer:**
- \( M = \) [input box] kN⋅m
[Button: eTextbook and Media]
[Button: Submit Answer]
---
**Part 4:**
Determine the maximum bending moment that can be applied to this cross section.
**Answer:**
- [Input box]
[Button: eTextbook and Media]
[Button: Submit Answer]
---
Note: No specific graphs or diagrams are present in the image to describe further.

Transcribed Image Text:The moment \( M \) acting on the cross section of the tee beam is oriented at an angle of \( \theta = 64^\circ \) as shown. Dimensions of the cross section are \( b_f = 245 \, \text{mm}, \, t_f = 22 \, \text{mm}, \, d = 279 \, \text{mm}, \, \text{and} \, t_w = 18 \, \text{mm} \). The allowable bending stress is 205 MPa. What is the largest bending moment \( M \) that can be applied as shown to this cross section?
### Diagram Explanation:
- **Diagram Layout**: The diagram depicts a tee beam cross section.
- **Labels**:
- \( A, B, C, D \): Points on the beam.
- \( b_f \): Width of the flange.
- \( t_f \): Thickness of the flange.
- \( d \): Overall depth of the beam.
- \( t_w \): Thickness of the web.
- \( y \): Distance from point \( A \) to the intersection of the web and flange.
- \( z \): Distance from point \( D \) horizontally to the intersection of the web and point where \( M \) is applied.
- \( \theta \): Angle at which moment \( M \) is applied.
- **Moment \( M \)**:
- Illustrated as a vector originating from point \( D \) at an angle \( \theta = 64^\circ \) with respect to the vertical axis.
The objective is to determine the maximum bending moment \( M \) that can be applied to this cross section without exceeding the allowable bending stress of 205 MPa.
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