Give step-by-step solution with explanation and final answer:Toe ht hon Fie 300m bn cn bigs 4d. kfc ti 8 a Eta hoof Be ct dh et Bra rg ond. Co oe memes ogc oe md eds om. Pro ibvarriet a e— ty en cro ion ig he spe mer od gr. Or dnd ofr mo er ep eng sr sr 1) puta ef ti poi on id com cin Figwe 1: Problem |
Question:
Give step-by-step solution with explanation and final answer:
Toe ht hon Fie 300m bn cn bigs 4d. kfc ti 8
a Eta hoof Be ct dh et
Bra rg ond. Co oe memes ogc oe md eds om.
Pro ibvarriet a e—
ty en cro ion ig he spe mer od gr.
Or dnd ofr mo er ep eng sr sr
1) puta ef ti poi on id com cin
Figwe 1: Problem |
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Asked by: Rahul
Created at: 2026-01-26 03:55:14
Asked by: Rahul
Created at: 2026-01-26 03:55:14
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Let's break down the problem step by step as requested:
---
# 1. Problem Summary
A shaft (200 mm long) is supported by bearings A and B. Belt forces (vertical and horizontal) act on a pulley at the center. The left end is attached to a clutch and transmits **torque**. Nothing is attached at the right end.
**Goal:** Calculate the stresses (normal and shear) at the critical cross-section (neglecting stress concentration).
---
# (a) **Identify the Critical Cross Section**
The shaft is subjected to:
- **Vertical Force:** 120 N (down)
- **Horizontal Force:** 200 N (to the right)
- **Torque:** 250 Nm (counterclockwise, as viewed from the right)
The **critical section** is the section where the combined stresses (bending + torsion) are *maximum*.
Since the forces and torque are applied at the pulley (center), **the critical cross-section is just to the left or right of the pulley** (i.e., at the center of the shaft, under the pulley).
---
# (b) **Sketch & Identify Points of Maximum Stress**
**Key Points on Cross-section:**
- **Top and Bottom fibers:** Maximum normal (bending) stress due to vertical force.
- **Left and Right fibers:** Maximum normal (bending) stress due to horizontal force.
- **Maximum Shear stress:** On the surface, at 45° from the neutral axis, due to torsion.
## **Types of Stresses:**
- **Bending normal stress:** due to vertical and horizontal forces
- **Shear stress:** due to torque (torsion)
---
# (c) **Populate the Stress Tensor for Analysis Points**
Let’s calculate the stresses at the **outer surface** at a point (for example, at the topmost fiber).
## **Given Data**
- Length between bearings: \( L = 200\, \text{mm} = .2\, \text{m} \)
- Diameter of shaft: \( d = 30\, \text{mm} = .03\, \text{m} \)
- Radius: \( r = \frac{d}{2} = .015\, \text{m} \)
- Vertical force: \( F_v = 120\,\text{N} \)
- Horizontal force: \( F_h = 200\,\text{N} \)
- Torque: \( T = 250\,\text{Nm} \)
---
## **Step 1: Calculate Bending Moments at the Center**
Since the forces are applied at the center, reactions at A and B will share the load equally.
### **Vertical Plane:**
- Each bearing reaction: \( R_v = \frac{F_v}{2} = 600\,\text{N} \)
- Moment at center: \( M_v = R_v \times (L/2) = 600\,\text{N} \times .1\,\text{m} = 60\,\text{Nm} \)
### **Horizontal Plane:**
- Each bearing reaction: \( R_h = \frac{F_h}{2} = 100\,\text{N} \)
- Moment at center: \( M_h = R_h \times (L/2) = 100\,\text{N} \times .1\,\text{m} = 100\,\text{Nm} \)
---
## **Step 2: Calculate Stresses**
### **Bending Stress, \( \sigma = \frac{M y}{I} \)**
Where:
- \( y = r = .015\,\text{m} \)
- \( I = \frac{\pi d^4}{64} = \frac{\pi (.03)^4}{64} = 3.98 \times 10^{-7} \, \text{m}^4 \)
#### **Vertical Bending:**
\[
\sigma_{bv} = \frac{M_v r}{I} = \frac{60 \times .015}{3.98 \times 10^{-7}} = 2.26 \times 10^6 \, \text{N/m}^2 = 2.26 \, \text{MPa}
\]
#### **Horizontal Bending:**
\[
\sigma_{bh} = \frac{M_h r}{I} = \frac{100 \times .015}{3.98 \times 10^{-7}} = 3.77 \times 10^6 \, \text{N/m}^2 = 3.77 \, \text{MPa}
\]
**Total bending stress at outer fiber (adding as vectors):**
\[
\sigma_b = \sqrt{(\sigma_{bv})^2 + (\sigma_{bh})^2} = \sqrt{(2.26)^2 + (3.77)^2} = 4.39 \, \text{MPa}
\]
---
### **Torsional (Shear) Stress, \( \tau = \frac{T r}{J} \)**
Where:
- \( J = \frac{\pi d^4}{32} = 2 \times I = 7.96 \times 10^{-7} \, \text{m}^4 \)
\[
\tau_{max} = \frac{T r}{J} = \frac{250 \times .015}{7.96 \times 10^{-7}} = 4.71 \times 10^6 \, \text{N/m}^2 = 4.71 \, \text{MPa}
\]
---
## **Step 3: Stress Tensor at Surface Point (e.g., Topmost Point)**
At the topmost fiber (due to vertical bending and torsion):
\[
\boxed{
\begin{bmatrix}
\sigma_b & \tau_{max} \\
\tau_{max} &
\end{bmatrix}
=
\begin{bmatrix}
4.39 & 4.71 \\
4.71 &
\end{bmatrix}
\, \text{MPa}
}
\]
- At the leftmost or rightmost fiber, the normal stress will be due to horizontal bending, and the shear stress due to torsion.
---
# **Summary Table**
| Point | Bending Stress (MPa) | Shear Stress (MPa) |
|-----------------|---------------------|--------------------|
| Top fiber | 4.39 | 4.71 |
| Bottom fiber | -4.39 | -4.71 |
| Side fibers | 3.77 | ±4.71 |
---
# **Final Answers**
### **(a)** *Critical cross-section*: At the center of the shaft, under the pulley.
### **(b)** *Points of max stresses*:
- Max normal stress at top/bottom and sides of the shaft cross-section.
- Max shear stress at the surface, at 45° to the axes (due to torsion).
### **(c)** *Stress tensor at top fiber*:
\[
\boxed{
\begin{bmatrix}
4.39 & 4.71 \\
4.71 &
\end{bmatrix}
\, \text{MPa}
}
\]
---
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