Difficulty: Medium
Correct Answer: 960 kg/cm^2
Explanation:
Introduction / Context:
This is a classic flexure problem for a simply supported member under a central point load. It tests the ability to compute section modulus and relate bending moment to extreme fiber stress.
Given Data / Assumptions:
Concept / Approach:
For a simply supported beam with a central load, maximum bending moment occurs at midspan and equals M_max = W * L / 4. The extreme fiber stress follows flexure formula: σ = M / Z, where Z is the section modulus of a rectangle, Z = b * d^2 / 6 (about the strong axis).
Step-by-Step Solution:
Compute M_max = W * L / 4 = 100 * 100 / 4 = 2500 kgf·cm.Compute section modulus Z = b * d^2 / 6 = 2.5 * (2.5)^2 / 6 = 15.625 / 6 = 2.6042 cm^3 (approx).Compute stress σ = M / Z = 2500 / 2.6042 ≈ 960 kg/cm^2.Therefore, the failure stress is about 960 kg/cm^2.
Verification / Alternative check:
Using more precise arithmetic yields the same rounded value (≈ 959.9 kg/cm^2). The answer aligns with typical cast iron flexural strength ranges.
Why Other Options Are Wrong:
980 and 1000 kg/cm^2 are overestimates from rounding errors; 1200 kg/cm^2 is significantly high for the given geometry and load.
Common Pitfalls:
Mixing N and kgf units; using I instead of Z directly; forgetting to convert L to centimeters when working in kg/cm^2.
Final Answer:
960 kg/cm^2
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