In case of a singly under-reinforced beam, the actual neutral Axis lies
above the critical neutral Axis
The question asks about the position of the actual neutral axis (NA) in a singly under-reinforced beam relative to the critical neutral axis. Understanding these concepts is key in reinforced concrete design.
The critical neutral axis, often called the balanced neutral axis, is a specific location within a beam's cross-section. It marks the point where the concrete reaches its maximum usable compressive strain (denoted as ${\epsilon}_{cu}$) at the same time the tensile steel reinforcement reaches its yield strain (denoted as ${\epsilon}_{y}$). A beam designed with the neutral axis at this position is called a balanced beam, and it exhibits a ductile failure mode.
The amount of tensile steel reinforcement determines the beam's classification and failure mode. This classification depends on how the actual neutral axis ($x_u$) compares to the critical neutral axis ($x_{cr}$):
| Beam Type | Reinforcement | Actual NA ($x_u$) vs Critical NA ($x_{cr}$) | Failure Mode |
| Under-reinforced | Less than balanced | $x_u < x_{cr}$ (Actual NA below critical NA) | Steel yields first (Ductile) |
| Over-reinforced | More than balanced | $x_u > x_{cr}$ (Actual NA above critical NA) | Concrete crushes first (Brittle) |
| Balanced | Balanced amount | $x_u = x_{cr}$ (Actual NA at critical NA) | Simultaneous failure |
For a singly under-reinforced beam, the design aims for the tensile steel to yield before the concrete crushes. Standard reinforced concrete theory dictates that this condition is met when the actual neutral axis lies below the critical neutral axis ($x_u < x_{cr}$).
The options provided are:
Option 2 is the correct choice.
For a simply supported beam or slab, the effective span is calculated as:
Which of the following is CORRECT for indeterminate beam condition?
A cantilever beam is one which is -
In case of deep beam or in thin webbed R.C.C members, the first crack formed is-
In case of web crippling, the dispersion of load from bearing plate takes place at: