Here are the steps to solve this problem:
1. Given:
Inlet diameter (d1) = 200 mm = 0.2 m
Throat diameter (d2) = 100 mm = 0.1 m
Specific gravity of oil (Sf) = 0.9
2. Calculate the areas:
Inlet area (A1) = πr12 = π(0.1)2 = 0.0314 m2
Throat area (A2) = πr22 = π(0.05)2 = 0.00785 m2
3. Use the venturimeter discharge equation:
Q = Cd * A1*