Experimental Study of a High-Frequency Fluidic Valve Fuel Injector

摘要

An' experimental study of a thrust vectoring system fit for unmanned air vehicle/unmanned combat air vehicle applications has been conducted. The influence of the cover-nozzle configuration on both the engine behavior and the vectoring performance has been checked. The most relevant conclusions of this work can be summarized as follows:rn1) The cover nozzle does not influence the engine functioning provided that its outlet section is high enough compared with the engine exhaust-nozzle one.