The deflection \( \delta \) at the centre of a simply supported beam subjected to a central concentrated load is given by the formula:
\[
\delta = \frac{W L^3}{48 E I}
\]
where:
- \( W \) is the applied load,
- \( L \) is the span of the beam,
- \( E \) is the Young's Modulus of the material,
- \( I \) is the moment of inertia of the beam's cross-section.
For a rectangular cross-section, the moment of inertia \( I \) is given by:
\[
I = \frac{b d^3}{12}
\]
where:
- \( b \) is the width of the beam,
- \( d \) is the depth of the beam.
If both the width and depth of the beam are doubled, the new moment of inertia becomes:
\[
I_{\text{new}} = \frac{(2b) (2d)^3}{12} = \frac{2b \cdot 8d^3}{12} = 8 \cdot \frac{b d^3}{12} = 8 I
\]
Since the deflection is inversely proportional to the moment of inertia, the new deflection will be:
\[
\delta_{\text{new}} = \frac{\delta}{8}
\]
Thus, the deflection at the centre of the beam will be reduced to \( \frac{1}{8} \) of the original deflection, which is 12.5% of the original deflection. Therefore, the correct answer is 6.25%.