Numerical and Experimental Investigations of Fluidic Thrust Vectoring with Oblique Shock Waves

摘要

FTV performance of the shock vector control method is evaluated for the 2D simple nozzle. Flow deflection angle evaluated from the momentum ratio depends much on where it is valuated. FTV performance is evaluated more directly with the pitching moment acting on the nozzle although it still has arbitrariness in the definition of the pivot location.