Math Problem Statement
A cantilever beam of rectangular cross-section is used to support a pulley. The tension in the wire rope is 5 KN. The beam is made of cast iron FG 200 and the factor of safety is 2.5. The ratio of depth to width of the cross-section is 2. Determine the dimensions of the cross-section of the beam
Solution
To solve this problem, let's analyze the situation and calculate the required dimensions of the cross-section of the beam. Here's the step-by-step procedure:
Given Data:
- Load on the beam due to tension in the rope:
- Length of the cantilever beam:
- Depth-to-width ratio:
- Material: Cast iron FG 200.
- Ultimate tensile strength
- Factor of Safety:
Step 1: Bending moment at the fixed end
The maximum bending moment occurs at the fixed end of the cantilever due to the applied load at the end:
Step 2: Allowable stress
The allowable bending stress is given by:
Step 3: Section modulus for the rectangular section
For a rectangular cross-section, the section modulus is:
Using the bending stress formula:
Substitute values:
Step 4: Dimensions of the cross-section
Using the section modulus formula , and the depth-to-width ratio , let . Substitute into :
Since :
Final Dimensions:
- Width (): 58.4 mm
- Depth (): 116.8 mm
Summary:
The dimensions of the cross-section of the beam are approximately:
- Width:
- Depth:
Would you like to see detailed explanations for any step or further clarifications? 😊
Related Questions:
- What is the importance of the factor of safety in design calculations?
- How is the bending stress distributed across a rectangular cross-section?
- Can the section modulus be improved without increasing the material volume?
- What is the significance of using FG 200 cast iron for this design?
- How would the design change if the depth-to-width ratio were altered?
Tip:
In beam design, maximizing the section modulus for a given material reduces stress and increases safety margins!
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Math Problem Analysis
Mathematical Concepts
Statics
Bending Moment
Allowable Stress
Section Modulus
Formulas
Maximum bending moment M = F × L
Allowable stress σ_allow = σ_ut / FOS
Section modulus Z = w × d^2 / 6
Z = M / σ_allow
Theorems
Bending Stress Formula
Section Modulus Relationship
Suitable Grade Level
Grades 11-12 / Engineering Foundation
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