Step 1: Find the diffuser's inlet and outlet areas.
The inlet radius matches the pipe, \(r_1 = 0.15\) m, so \(A_1 = \pi r_1^2 = \pi(0.15)^2 = 0.07069\) m\(^2\). At the outlet, \(x = 0.5\) m, so \(r_2 = 0.15 + 0.4(0.5)^2 = 0.15+0.1 = 0.25\) m, giving \(A_2 = \pi(0.25)^2 = 0.19635\) m\(^2\).
Step 2: Get the velocities from the flow rate.
\(Q = 4.5\) m\(^3\)/min \(= 0.075\) m\(^3\)/s. Then \(V_1 = Q/A_1 = 0.075/0.07069 = 1.061\) m/s and \(V_2 = Q/A_2 = 0.075/0.19635 = 0.382\) m/s.
Step 3: Use Bernoulli's equation to get the inlet gauge pressure.
Since the diffuser is frictionless and horizontal and the outlet reaches atmospheric pressure (\(p_2 = 0\) gauge), \(p_1 + \tfrac12\rho V_1^2 = p_2 + \tfrac12\rho V_2^2\), so \(p_1 = \tfrac12\rho(V_2^2-V_1^2) = 500(0.382^2-1.061^2) = 500(0.1459-1.1258) = -489.9\) Pa. The negative sign shows the inlet pressure sits below atmospheric, as expected since the diffuser is raising the pressure up to atmospheric.
Step 4: Apply the linear momentum equation on the water inside the diffuser.
Taking the flow direction as positive, the net force \(F_R\) that the flange applies on the fluid, plus the inlet pressure force, minus the outlet pressure force, equals the momentum change: \(p_1 A_1 - p_2 A_2 + F_R = \dot{m}(V_2-V_1)\), where \(\dot m = \rho Q = 1000(0.075) = 75\) kg/s.
\(\dot m (V_2-V_1) = 75(0.382-1.061) = -50.93\) N.
\(F_R = \dot m(V_2-V_1) - p_1A_1 + p_2A_2 = -50.93 - (-489.9)(0.07069) + 0 = -50.93+34.63 = -16.30\) N.
Step 5: Apply Newton's third law.
\(F_R\) is the force the flange applies on the fluid to hold the diffuser in place. By Newton's third law, the diffuser pushes back on the flange with the same magnitude in the opposite sense.
Final Answer:
The magnitude of the force the diffuser exerts on the flange comes straight from the momentum balance across the diverging section.
\[ \boxed{F = 16.30 \ \text{N}} \]