| Abstract: | A method is proposed for the numerical-analytic design of a high-lift airfoil with slit air suction from the external flow within the framework of ideal fluid theory. The suction slit is represented by a channel with constant wall velocity. Examples of the design of wing profiles with non-detached flows having lift coefficientsCy=2.68 and 4 and maximum relative velocities over the profile [ max|/ =2 and 2.2 are given. A scheme for an aircraft of the  flying wing type with internally located engines and pay load is briefly discussed.Kazan', Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 6, pp. 23–28, November–December, 1996. |
