Invention Grant
US09551296B2 Method and apparatus for nozzle thrust vectoring 有权
喷嘴推力矢量的方法和装置

Method and apparatus for nozzle thrust vectoring
Abstract:
A thrust vectoring system is created with a convergent-divergent nozzle having a total angle no greater than 150 degrees. A divergent portion of the nozzle has a wall at a predetermined angle of at least 12° from the freestream direction. A disturbance generator is located on the wall to induce flow separation from the wall with the predetermined wall angle sufficient for the induced flow separation to extend upstream from disturbance generator substantially to a throat of the nozzle pressurizing the wall and creating a net vector angle in jet flow through the nozzle.
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