Gas-Turbine Powerplants For Two-Phase Hydropropulsion 



0.8 



OA 



^ 



(a) 



Of, op 



lA 1.6 



(b) 



Fig, 13 - Variation of the specific thrust a 

 and its value a^ corresponding to throat 

 truncation (y = 0.9, a. p.) 



1125 



