Control of the Periodic Turbulent Flow over a Semicircular Airfoil with the Use of the Slot Suction of the Air from a Circular Vortex Cell at Small Angles of Attack
It is shown that, in the case where, into the back wall of a semicircular airfoil with an angle of attack of 5°, a vortex cell of diameter 0.2 in fractions of the airfoil chord is built in and the mean-mass rate of slot suction of the air from this cell is larger than 0.15 of the incident-flow veloc...
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Veröffentlicht in: | Journal of engineering physics and thermophysics 2016-11, Vol.89 (6), p.1500-1504 |
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description | It is shown that, in the case where, into the back wall of a semicircular airfoil with an angle of attack of 5°, a vortex cell of diameter 0.2 in fractions of the airfoil chord is built in and the mean-mass rate of slot suction of the air from this cell is larger than 0.15 of the incident-flow velocity, the pattern of the turbulent flow over the airfoil is transformed, and, at an optimum suction rate of 0.75, the lift coefficient of the airfoil reaches a maximum value of the order of 1.7 at an aerodynamic efficiency of 10. |
doi_str_mv | 10.1007/s10891-016-1519-0 |
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subjects | Aerodynamics Airfoils Classical Mechanics Complex Systems Engineering Engineering Thermodynamics Fluid dynamics Fluid flow Heat and Mass Transfer Hydrogasdynamics in Technological Processes Industrial Chemistry/Chemical Engineering Suction Thermodynamics Turbulence Turbulent flow Vortices |
title | Control of the Periodic Turbulent Flow over a Semicircular Airfoil with the Use of the Slot Suction of the Air from a Circular Vortex Cell at Small Angles of Attack |
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