When the section is subjected to an axial load and a moment, the ratio of the moment to the load is called:
Eccentricity
When a structural section is subjected to forces, these forces can cause various types of stresses. An axial load is a force acting along the longitudinal axis of the member. A moment is a rotational effect caused by a force acting at a distance.
Often, a section is subjected to both an axial load and a moment simultaneously. This happens when the applied load is not acting perfectly through the centroid of the section. When the load acts away from the centroid, it is called an eccentric load.
Eccentricity is defined as the distance between the point of application of the axial load and the centroid of the section. An eccentric load 'P' acting at a distance 'e' from the centroid creates a moment 'M'. This moment is calculated as the product of the load and the eccentricity.
The formula for the moment is:
\( M = P \times e \)
Where:
We are asked about the ratio of the moment to the load, which is \( \frac{M}{P} \). From the formula \( M = P \times e \), we can rearrange it to find this ratio:
\( \frac{M}{P} = e \)
Therefore, the ratio of the moment to the axial load is equal to the eccentricity.
Based on the relationship \( \frac{M}{P} = e \), the ratio of the moment to the axial load is known as eccentricity.
For a simply supported beam carrying distributed load w per unit length, consider the following relations between shear force F and bending moment M.
A. \(\rm w=-\frac{dF}{dx}\)
B. \(\rm w=-\frac{d^2M}{dx^2}\)
C. \(\rm F=\frac{dM}{dx}\)
Which of the above statements is/are correct ?
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For a cantilever beam of length 2 m, under load of 1 kN/m, the maximum bending moment is