Act like a helpful tutor and exlain me :
Give step-by-step solution with explanation and final answer:A beam fabricated from western white pine
has been reinforced by bonding steel strips
on its top and bottom surfaces as shown. If
the design is limited to 0'y00¢ = 1.6 ksi in the
wood and see; = 35.7 ksi in the steel,
determine the maximum bending moment if
the beam bends about its vertical axis of
symmetry.
L
~ : =] L,
' —
[ry
STEEL f
Ly
WOOoD
: y —
N.A. L,
Given:
« L; =10.7in
« Ly=16in
« Ly=4.1in
Maz = number (it kip-in @
Question:
Act like a helpful tutor and exlain me :
Give step-by-step solution with explanation and final answer:A beam fabricated from western white pine
has been reinforced by bonding steel strips
on its top and bottom surfaces as shown. If
the design is limited to 0'y00¢ = 1.6 ksi in the
wood and see; = 35.7 ksi in the steel,
determine the maximum bending moment if
the beam bends about its vertical axis of
symmetry.
L
~ : =] L,
' —
[ry
STEEL f
Ly
WOOoD
: y —
N.A. L,
Given:
« L; =10.7in
« Ly=16in
« Ly=4.1in
Maz = number (it kip-in @
This is AI generated Response.
Asked by: manish kumar
Created at: 2025-10-08 10:06:35
Final Answer:
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Let's solve the problem step by step.
---
## **Step 1: Understand the Problem**
We have a composite beam (wood + steel strips) subjected to bending. The maximum bending moment is limited by the allowable stresses in wood (\(\sigma_{wood}\)) and steel (\(\sigma_{steel}\)).
**Given:**
- \(\sigma_{wood} = 1.6\) ksi
- \(\sigma_{steel} = 35.7\) ksi
- \(L_1 = 10.7\) in (height of wood)
- \(L_2 = 1.6\) in (height of steel strip)
- \(L_3 = 4.1\) in (width of beam)
---
## **Step 2: Find the Modular Ratio**
The modular ratio (\(n\)) compares the modulus of elasticity of steel (\(E_s\)) to that of wood (\(E_w\)). Typically:
- \(E_{steel} \approx 29,000\) ksi
- \(E_{wood} \approx 1,200\) ksi (for pine)
\[
n = \frac{E_{steel}}{E_{wood}} = \frac{29,000}{1,200} \approx 24.17
\]
---
## **Step 3: Transform the Section**
Convert the steel strip areas to an equivalent wood area using the modular ratio.
- **Width of the beam:** \(b = L_3 = 4.1\) in
- **Area of one steel strip:** \(A_{steel} = b \times L_2 = 4.1 \times 1.6 = 6.56 \, \text{in}^2\)
Equivalent area in wood:
\[
A_{steel,eq} = n \times A_{steel} = 24.17 \times 6.56 \approx 158.6 \, \text{in}^2
\]
---
## **Step 4: Locate the Neutral Axis**
Let’s place the bottom of the beam at \(y = \).
- **Wood:** From \(y = L_2\) to \(y = L_2 + L_1\)
- **Top steel:** From \(y = L_2 + L_1\) to \(y = 2L_2 + L_1\)
- **Bottom steel:** From \(y = \) to \(y = L_2\)
Calculate centroid (\(\bar{y}\)) of the equivalent section:
\[
\text{Total Area} = A_{wood} + 2A_{steel,eq}
\]
\[
A_{wood} = b \times L_1 = 4.1 \times 10.7 = 43.87 \, \text{in}^2
\]
\[
\text{Total Area} = 43.87 + 2 \times 158.6 = 361.07 \, \text{in}^2
\]
Calculate the first moment of area about bottom:
\[
Q = A_{wood} \cdot y_{wood} + 2 \cdot A_{steel,eq} \cdot y_{steel}
\]
Where:
- \(y_{wood}\) = distance from bottom to centroid of wood = \(L_2 + \frac{L_1}{2} = 1.6 + 5.35 = 6.95\) in
- \(y_{steel, bottom}\) = centroid of bottom steel = \(.8\) in
- \(y_{steel, top}\) = centroid of top steel = \(L_2 + L_1 + .8 = 1.6 + 10.7 + .8 = 13.1\) in
\[
Q = (43.87 \times 6.95) + (158.6 \times .8) + (158.6 \times 13.1)
\]
\[
Q = 305.89 + 126.88 + 2077.66 = 251.43
\]
\[
\bar{y} = \frac{Q}{\text{Total Area}} = \frac{251.43}{361.07} \approx 6.95 \, \text{in}
\]
---
## **Step 5: Calculate Moment of Inertia (\(I_{trans}\))**
Moment of inertia for each part (about neutral axis):
1. **Wood:**
\[
I_{wood} = \frac{b L_1^3}{12} + A_{wood} (y_{wood} - \bar{y})^2
\]
\[
= \frac{4.1 \times 10.7^3}{12} + 43.87 \times (6.95 - 6.95)^2
\]
\[
= \frac{4.1 \times 1224.3}{12} = \frac{502}{12} = 418.3 \, \text{in}^4
\]
2. **Steel (bottom):**
\[
I_{steel, bottom} = \frac{b L_2^3}{12} + A_{steel,eq} (y_{steel, bottom} - \bar{y})^2
\]
\[
= \frac{4.1 \times 1.6^3}{12} + 158.6 \times (.8 - 6.95)^2
\]
\[
= \frac{4.1 \times 4.096}{12} = 1.4 + 158.6 \times 37.82 = 1.4 + 6001.85 = 6003.25 \, \text{in}^4
\]
3. **Steel (top):**
\[
I_{steel, top} = \frac{4.1 \times 1.6^3}{12} + 158.6 \times (13.1 - 6.95)^2
\]
\[
= 1.4 + 158.6 \times 37.82 = 1.4 + 6001.85 = 6003.25 \, \text{in}^4
\]
\[
I_{trans} = 418.3 + 6003.25 + 6003.25 = 12424.8 \, \text{in}^4
\]
---
## **Step 6: Find Maximum Moment Based on Allowable Stresses**
The maximum moment is found by checking both materials:
\[
M = \frac{\sigma I}{c}
\]
where \(c\) is the distance from the neutral axis to the extreme fiber.
- **For wood:** \(c_{wood} = \bar{y} - (L_2) = 6.95 - 1.6 = 5.35\) in
- **For steel (top):** \(c_{steel} = (L_2 + L_1 + L_2) - \bar{y} = (1.6 + 10.7 + 1.6) - 6.95 = 13.9 - 6.95 = 6.95\) in
### **A. Wood Controls**
\[
M_{wood} = \frac{\sigma_{wood} I_{trans}}{c_{wood}}
\]
\[
M_{wood} = \frac{1.6 \times 12424.8}{5.35} = \frac{19879.68}{5.35} = 3718.6 \, \text{kip-in}
\]
### **B. Steel Controls**
*Remember, the steel area was multiplied by \(n\), so we must use the actual steel stress:*
\[
M_{steel} = \frac{\sigma_{steel} I_{trans}}{n \cdot c_{steel}}
\]
\[
M_{steel} = \frac{35.7 \times 12424.8}{24.17 \times 6.95}
\]
\[
= \frac{444,367.36}{168.92} = 2631.1 \, \text{kip-in}
\]
---
## **Step 7: Final Answer**
The maximum allowable moment is the **lower** of the two:
\[
\boxed{M_{max} = 263 \ \text{kip-in}}
\]
(Rounded to 3 significant digits.)
---
### **Summary Table**
| Material | Allowable Moment (kip-in) |
|----------|--------------------------|
| Wood | 3719 |
| Steel | 263 |
**Final Answer:**
\[
\boxed{M_{max} = 263 \ \text{kip-in}}
\]
Let me know if you want any step clarified further!
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