吹き出し翼における境界層はく離制御に必要な

吹き出し運動量の計算について

抄録

The present paper deals with a calculation method of the value of the jet momentum required to control the separation position of the twodimensional incompressible air flow with the turbulent boundary layer along the wing (or body) surface by a tangential air jet discharged from a slit equipped on it. And moreover, the effects of Reynolds number and the ratio of the slit width to the wing (or body) chord as well as those of the profile and incidence of the wing (or body), the attached distance of the external flow and the slit position, on the required jet momentum are discussed.