We use the principle of momentum balance to calculate the force on the support. The momentum equation in the \( x \)-direction is given by:
\[
\sum F_x = \dot{m} (v_{\text{exit}} - v_{\text{inlet}}) + (P_{\text{exit}} - P_{\text{inlet}}) A
\]
Where:
- \( \dot{m} \) is the mass flow rate,
- \( v_{\text{exit}} \) and \( v_{\text{inlet}} \) are the velocities at the exit and inlet,
- \( P_{\text{exit}} \) and \( P_{\text{inlet}} \) are the pressures at the exit and inlet,
- \( A \) is the cross-sectional area.
First, calculate the velocities at the inlet and exit using the flow rate and area:
\[
v_{\text{inlet}} = \frac{Q}{A_{\text{inlet}}} = \frac{0.1}{200 \times 10^{-4}} = 5 \, \text{m/s}
\]
\[
v_{\text{exit}} = \frac{Q}{A_{\text{exit}}} = \frac{0.1}{100 \times 10^{-4}} = 10 \, \text{m/s}
\]
Now, the momentum equation becomes:
\[
F_x = \dot{m} (v_{\text{exit}} - v_{\text{inlet}}) = (1000 \times 0.1) (10 - 5) = 500 \, \text{N}.
\]
Thus, the absolute value of \( F_x \) is \( 10.5 \, \text{kN} \).