Abstract:Controlling and redirecting the low-kinetic-energy layers of flow on the fuselage of aircrafts, is one of the most demanding stages in the advanced aerodynamic designs. Among the applications, Inlet/body integration needs the serious considerations to prevent the boundary layer from being swallowed by the inlet entrance. Not only the classic diverters are outclass nowadays, but also the newly used bump surfaces have still faced some problems under the effects of thick boundary layer. In this paper a new concep… Show more
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