Act like a helpful tutor and exlain me :
Give step-by-step solution with explanation and final answer:A steel bar of thickness his welded 10 a vertical support as shown In the figure. Find the safe force F If the maximum allowable shear
ress Inthe Welds rupee -
hv
i
WN,
where b= 3.750 in, c = 5.80 in, d = 1.800 in, h = 0.3125 in, and Tanew ~ 25 kpsi
The safe force s [Tp
Question:
Act like a helpful tutor and exlain me :
Give step-by-step solution with explanation and final answer:A steel bar of thickness his welded 10 a vertical support as shown In the figure. Find the safe force F If the maximum allowable shear
ress Inthe Welds rupee -
hv
i
WN,
where b= 3.750 in, c = 5.80 in, d = 1.800 in, h = 0.3125 in, and Tanew ~ 25 kpsi
The safe force s [Tp
This is AI generated Response.
Asked by: manish kumar
Created at: 2025-09-21 11:29:13
Final Answer:
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Let's solve the problem step by step:
---
## **Given Data**
- \( b = 3.750 \) in
- \( c = 5.80 \) in
- \( d = 1.800 \) in
- \( h = 0.3125 \) in
- \( \tau_{allow} = 25 \) ksi = 25,000 psi
---
## **Step 1: Find the Total Weld Length**
The weld is around three sides (left, top, and right):
\[
\text{Total Weld Length (L)} = b + 2c
\]
\[
L = 3.75 + 2 \times 5.80 = 15.35\ \text{in}
\]
---
## **Step 2: Find Weld Throat Area**
The throat of a fillet weld is:
\[
\text{Throat} = 0.707h
\]
\[
\text{Area} = \text{Total Weld Length} \times \text{Throat}
\]
\[
\text{Area} = 15.35 \times 0.707 \times 0.3125 = 3.397\ \text{in}^2
\]
---
## **Step 3: Shear due to the Applied Force \( F \) (Direct Shear)**
\[
\tau_{direct} = \frac{F}{\text{Weld Area}}
\]
---
## **Step 4: Shear due to Moment (Eccentric Load)**
The force \( F \) is applied at a distance \( d \) from the weld centroid, producing a moment:
\[
M = F \times d
\]
Each infinitesimal segment of weld resists a part of this moment as secondary shear.
The maximum secondary shear stress occurs at the farthest point from the centroid.
For a rectangular weld group (approximate method):
\[
r_{max} = \sqrt{\left(\frac{b}{2}\right)^2 + c^2}
\]
\[
J = \sum (l_i r_i^2)
\]
Since weld group is symmetric:
\[
J = \frac{b^3}{12} + b \left(\frac{c}{2}\right)^2 + 2\left[\frac{c^3}{12} + c \left(\frac{b}{2}\right)^2\right]
\]
But for simplicity, since the weld is three sides (U-shape), let's use:
\[
J = \sum l_i r_i^2
\]
For each side:
- Bottom: \( b \) at \( r = c \)
- Sides: \( c \) at \( r = \sqrt{(b/2)^2 + c^2} \)
But let's use a simplified version for classroom problems:
\[
J = b c^2 + 2c \left[ \left(\frac{b}{2}\right)^2 \right]
= b c^2 + c b^2/2
\]
---
## **Step 5: Maximum Shear Stress**
The resultant shear stress at the most critical point:
\[
\tau_{max} = \sqrt{ \left(\tau_{direct}\right)^2 + \left(\tau_{secondary}\right)^2 + 2 \tau_{direct} \tau_{secondary} \cos \theta }
\]
But if the directions are perpendicular, usually:
\[
\tau_{max} = \tau_{direct} + \tau_{secondary}
\]
---
## **Step 6: Set \( \tau_{max} = \tau_{allow} \) and Solve for \( F \)**
Let's perform the calculations step-by-step.
---
### **Detailed Calculations**
#### **Weld Length**
\[
L = b + 2c = 3.75 + 2 \times 5.80 = 15.35\ \text{in}
\]
#### **Throat Area**
\[
A = L \times 0.707 \times h = 15.35 \times 0.707 \times 0.3125 = 3.397\ \text{in}^2
\]
#### **Shear due to Force \( F \)**
\[
\tau_{direct} = \frac{F}{3.397}
\]
#### **Location of Centroid**
For a U-shape weld, the centroid is offset from the left edge. But for this calculation, let's take the distance from the centroid to where \( F \) acts:
\[
r_{max} = \sqrt{(b/2)^2 + c^2}
= \sqrt{(3.75/2)^2 + (5.80)^2}
= \sqrt{(1.875)^2 + (5.80)^2}
= \sqrt{3.516 + 33.64}
= \sqrt{37.156}
= 6.10\ \text{in}
\]
#### **Polar Moment of Weld Group (\( J \)):**
For a U-shaped weld:
\[
J \approx b c^2 + \frac{b^3}{6}
= 3.75 \times (5.80)^2 + \frac{(3.75)^3}{6}
= 3.75 \times 33.64 + \frac{52.73}{6}
= 126.15 + 8.79
= 134.94\ \text{in}^3
\]
#### **Secondary Shear due to Moment**
\[
\tau_{secondary} = \frac{M r_{max}}{J \cdot \text{throat}}
= \frac{F d r_{max}}{J A / L}
\]
But, using the more common formula:
\[
\tau_{secondary} = \frac{M r_{max}}{J \cdot \text{throat}}
= \frac{F d r_{max}}{J \cdot 0.707 h}
\]
But since \( A = L \times 0.707 h \), and \( J \) is as above:
\[
\tau_{secondary} = \frac{F d r_{max}}{J \cdot 0.707 h}
\]
Plug in values:
- \( d = 1.8 \) in
- \( r_{max} = 6.10 \) in
- \( J = 134.94 \) in\(^3\)
- \( h = 0.3125 \) in
\[
\tau_{secondary} = \frac{F \times 1.8 \times 6.10}{134.94 \times 0.707 \times 0.3125}
\]
\[
= \frac{F \times 10.98}{29.89}
= 0.3675 F
\]
#### **Total Shear**
\[
\tau_{max} = \tau_{direct} + \tau_{secondary}
= \frac{F}{3.397} + 0.3675 F
\]
Set \( \tau_{max} = \tau_{allow} = 25,000 \) psi:
\[
\frac{F}{3.397} + 0.3675 F = 25,000
\]
\[
F \left( \frac{1}{3.397} + 0.3675 \right) = 25,000
\]
\[
\frac{1}{3.397} = 0.2943
\]
\[
0.2943 + 0.3675 = 0.6618
\]
\[
0.6618 F = 25,000
\]
\[
F = \frac{25,000}{0.6618} = 37,781 \ \text{lbf}
\]
---
### **Step 7: Convert to kips**
\[
1 \ \text{kip} = 1,000 \ \text{lbf}
\]
\[
F = \frac{37,781}{1,000} = 37.8 \ \text{kip}
\]
---
## **Final Answer**
**The safe force is:**
\[
\boxed{37.8 \ \text{kip}}
\]
---
### **Summary Table**
| Step | Value |
|------------------------------|-------------|
| Total weld length \( L \) | 15.35 in |
| Weld throat area \( A \) | 3.397 in² |
| Polar moment \( J \) | 134.94 in³ |
| Max distance \( r_{max} \) | 6.10 in |
| Allowable shear \( \tau_{allow} \) | 25 ksi = 25,000 psi |
| **Safe force \( F \)** | **37.8 kip**|
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