The beam is subjected to a uniformly distributed load, and we are tasked with finding the curvature at the fixed end of the cantilever beam. The curvature \( \kappa \) at any point on the beam is given by the equation:
\[
\kappa = \frac{M(x)}{EI}
\]
where:
- \( M(x) \) is the bending moment at a point \( x \) on the beam,
- \( E \) is the Young's modulus of the material (we are given the bending rigidity \( C = EI \)),
- \( I \) is the second moment of area, which together with \( E \) gives the bending rigidity \( C \).
Step 1: Calculate the bending moment
For a cantilever beam with a uniformly distributed load \( C \), the bending moment at a distance \( x \) from the fixed end is:
\[
M(x) = \frac{C x^2}{2}
\]
Substituting \( C = 10 \, \text{kN/m} \) and \( x = 0.3 \, \text{m} \):
\[
M(0.3) = \frac{10 \times (0.3)^2}{2} = \frac{10 \times 0.09}{2} = 0.45 \, \text{kN}\cdot\text{m}.
\]
Step 2: Calculate the curvature at the fixed end
The bending rigidity is given as \( C = 5000 \, \text{Nm}^2 \). So, using the formula for curvature at the fixed end (\( x = 0 \)):
\[
\kappa = \frac{M(0)}{C} = \frac{0.45}{5000} = 0.00009 \, \text{m}^{-1}.
\]
Thus, the magnitude of the curvature at the fixed end is \( 0.09 \, \text{m}^{-1} \), so the correct answer is (C).