and C are arranged such that when the power jet deflects, the x 

 CD-ordinate of each point is x^ . The output ports layout is such that 

 the power jet axis coincides with that of the Port Ol. Thus angle of 

 the port 0^ axis is equal to ^o as shown in Figure 24, Further, the 

 width, w , of each port is derived from Equation (3-b) as 



57.3 



(12) 



where 



= maximum dimensionless control flow corresponding 

 to the maximum deflection, 

 jet. 



AUi , of the power 

 max 



57.3 = a factor for converting degrees into radians 

 X = CD-ordinate of the splitter tip 



o r r 



As an illustration Table 5 give the values of output port, w , for 

 Xq = 3 and 4 inches respectively for various combinations of the 

 active and passive legs Q^^ and Qp. The angular location of the output 

 port is achieved on the basis of the power jet emanating angle with 

 no control flow, i.e., ^ . This angle for various combinations of 

 the active and passive leg flows was measured and recorded in Table 3. 

 Further, the co-ordinates of points A, B, and C change with the control 

 flow and can be obtained using Equation (12). These are given below: 



X = X (13-a) 



2 X 57.3 



(13-b) 

 (13-c) 



2 X 57.3 



^' q: 



and (13-d) 



(13-e) 



15 



