Improving the Lift Properties of a Wing in Takeoff and Landing by Means of a Boundary Layer Control System Using Ejector-Type Actuators
A device making it possible to control of the flow past a wing at low flight speeds is proposed. The device comprises an ejector-type actuator that simultaneous sucks the boundary layer on the upper surface and blows a gas jet in the vicinity of the trailing edge. Based on the Reynolds-averaged Navi...
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Veröffentlicht in: | Technical physics letters 2018-08, Vol.44 (8), p.687-690 |
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creator | Voevodin, A. V. Kornyakov, A. A. Petrov, D. A. Petrov, A. S. Sudakov, G. G. |
description | A device making it possible to control of the flow past a wing at low flight speeds is proposed. The device comprises an ejector-type actuator that simultaneous sucks the boundary layer on the upper surface and blows a gas jet in the vicinity of the trailing edge. Based on the Reynolds-averaged Navier–Stokes equations, a mathematical model of an ejector-type actuator is developed and experimental studies are carried out. |
doi_str_mv | 10.1134/S106378501808014X |
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V.</creatorcontrib><creatorcontrib>Kornyakov, A. A.</creatorcontrib><creatorcontrib>Petrov, D. A.</creatorcontrib><creatorcontrib>Petrov, A. S.</creatorcontrib><creatorcontrib>Sudakov, G. G.</creatorcontrib><collection>CrossRef</collection><collection>OSTI.GOV</collection><jtitle>Technical physics letters</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Voevodin, A. V.</au><au>Kornyakov, A. A.</au><au>Petrov, D. A.</au><au>Petrov, A. S.</au><au>Sudakov, G. G.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Improving the Lift Properties of a Wing in Takeoff and Landing by Means of a Boundary Layer Control System Using Ejector-Type Actuators</atitle><jtitle>Technical physics letters</jtitle><stitle>Tech. Phys. 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subjects | Actuators Boundary layer Boundary layer control BOUNDARY LAYERS Classical and Continuum Physics Computational fluid dynamics COMPUTERIZED SIMULATION CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY CONTROL SYSTEMS Ejection EQUATIONS Gas jets NAVIER-STOKES EQUATIONS Physics Physics and Astronomy Reynolds averaged Navier-Stokes method REYNOLDS NUMBER SURFACES |
title | Improving the Lift Properties of a Wing in Takeoff and Landing by Means of a Boundary Layer Control System Using Ejector-Type Actuators |
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