Frictional drag occupies a large proportion in the resistance of modern civil aircraft,and the understanding of the generation mechanism of frictional drag is the basis of the turbulence drag reductio
A passive flow control method,which is to use an inclined controlling hole(CH)passing through the free-end surface to the side of the rear surface,was developed for a circular cylinder of an aspect ra
In order to understand the controlling mechanism using plasma actuator and develop the mathematical model of plasma actuator,the turbulent characteristics of the jet induced by a Dielectric Barrier Di
The previous research has demonstrated the ability of alternating current dielectric barrier discharge(AC-DBD)plasma actuation to manipulate the asymmetric vortex fields over a conical forebody[1].
The unsteady loads and flow field on a maneuvering aircraft considerably differ from static conditions,especially for configurations incorporating vortex flow.In this article,dynamic motions of a nons