Answer:
The value is
Explanation:
From the question we are told that
The flow rate is 
The entrance diameter is 
The exit diameter is evaluated as
The entrance gauge pressure is 
The droped gauge pressure is 
The presure at the exist is evaluated as 
Generally the entrance cross-sectional area is mathematically represented as



Generally the exit cross-sectional area is mathematically represented as



Generally from the continuity equation

=>
=>
=>
Generally the net force in horizontal axis is equivalent to the net momentum change in the horizontal direction
So
![P_g * A + F_t - P_e * A_e = P_d [ A_e * v_2^2 - A* v_1^2]](https://tex.z-dn.net/?f=P_g%20%2A%20%20A%20%2B%20%20F_t%20-%20P_e%20%2A%20%20A_e%20%20%3D%20%20P_d%20%5B%20A_e%20%2A%20v_2%5E2%20-%20%20A%2A%20v_1%5E2%5D)
Here
is the horizontal thrust on the fitting
So
![350*10^{3} * 0.385 + F_t -0.385 * 0.139 = 50*10^{3} [ 0.385* 13.8^2 - 0.385* 5^2]](https://tex.z-dn.net/?f=350%2A10%5E%7B3%7D%20%2A%200.385%20%20%2B%20%20F_t%20-0.385%20%20%2A%20%200.139%20%20%3D%20%2050%2A10%5E%7B3%7D%20%5B%200.385%2A%2013.8%5E2%20-%20%200.385%2A%205%5E2%5D)