the power jet velocity from Equation (7) and the jet configuration 

 from Figure 24, the flow Q through the output port is 



^h 2 / \ 



QqL = / h U(x^) Sech ^f^ j dy (15) 



and the flow Q through the output port is 

 OR K 



'OR 



/ 



h U(x ) Sech ( ^^ ) dy 



(f) 



(16) 



Further by integrating Equations (15) and (16) and using Equations 

 (13-a) throiji^ (13-f ) for value of y , y , and y , one obtains 



U(x )x h 

 Q = o o 

 ^OL = 



I- max J L ma 



+ 2(Q,/Q,) 



(17) 



and U(x^)xQh 

 ^OR = 



tanh 



gs 



L max 



tanh 



gs 



114.6 



(Q /Q ) - 2 (Q /Q ) 

 c a c a 



(18) 



Further, recall from Equation (11-b) that 



P = 



U(x)hVxw U(x )h Jx w 

 '^ a ^o^oa 



(19) 



17 



