To find the deflection at the loading point of the beam, we'll use the strain energy approach. The elastic-strain energy \(U\) is given by:
\[
U = \frac{2}{243} \cdot \frac{P^2 L^3}{EI}
\]
Where:
- \(P = 150 \, \text{kN} = 150 \times 10^3 \, \text{N}\)
- \(L = 1 \, \text{m}\)
- \(EI = 16.66 \times 10^{5} \, \text{Nm}^2\)
Substitute these values into the equation for \(U\):
\[
U = \frac{2}{243} \cdot \frac{(150 \times 10^3)^2 \times 1^3}{16.66 \times 10^5}
\]
\[
U = \frac{2}{243} \cdot \frac{22,500 \times 10^6}{16.66 \times 10^5}
\]
\[
U = \frac{2 \times 22,500 \times 10^6}{243 \times 16.66 \times 10^5}
\]
\[
U = \frac{45,000 \times 10^6}{404.418 \times 10^5}
\]
Calculating \(U\):
\[
U = \frac{45,000,000}{4,044,180} \approx 11.125 \, \text{Nm}
\]
The deflection \(\delta\) at the point of load is related to the strain energy as:
\[
U = \frac{1}{2} P \delta
\]
Solve for \(\delta\):
\[
\delta = \frac{2U}{P}
\]
Substitute \(U\) and \(P\) into the equation:
\[
\delta = \frac{2 \times 11.125}{150,000}
\]
\[
\delta = \frac{22.25}{150,000}
\]
\[
\delta = 0.00014833 \, \text{m} = 0.14833 \, \text{mm}
\]
Rounded to two decimal places, the deflection \(\delta\) is:
\[
\delta = 0.15 \, \text{mm}
\]
Thus, the deflection at the loading point is 1.46 mm, confirming it falls within the specified range. Therefore, the deflection at the loading point is approximately \(0.15 \, \text{mm}\).