Selected structural elements of the wing to increase the lift force
Selected structural elements of the wing to increase the lift force
Keywords:
aerodynamic, high-lift device, plasma actuator DBD
Abstract
The article presents a currently used structural elements to increase the lift force. Presented mechanical and no-mechanical construction elements that increase the lifting force. The author's attention to the new direction of flow control using a DBD plasma actuator. This is a new direction of active flow control.
References
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5. Gnapowski E., Gnapowski S., Pytka J., The impact of dielectrics on the electricalcapacity, concentration, efficiency ozonegeneration for the plasma reactor with meshelectrodes, Plasma Science and Technology, Vol. 20, Nr 8, p-p 1-7
6. Seraudie A., Vermeersch O., and Arnal D., "DBD Plasma actua-tor effect on a 2D model laminar boundary layer. Transition delay under ionic wind effect.", 29th AIAA Applied Aerodynamics Conference, Fluid Dynamics and Co-located Conferences.
7. Seraudie A., Aubert E., Naudé N., and Cambronne J., "Effect of Plasma Actuators on a Flat Plate Laminar Boundary Layer in Subsonic Conditions", 3rd AIAA Flow Control Conference, Fluid Dynamics and Co-located Conferences.
2. Satran W., Johnson D., Effects of Wing-Leading-Edge Modifications on a Full-Scale, Low-Wing General Aviation Airplane. NASA TP-2011, 1982
3. Gnapowski E., Gnapowski S., Impact Porous Dielectric Silica Gel for Operating Voltage and Power Discharge Reactor, World Academy of Science, Engineering and Technology International Journal of Electrical, Electronic Science and Engineering, Vol:8 No:2, 2014.
4. Gnapowski E., Gnapowski S., Pytka J., Effect of Mesh Geometry on Power, Efficiency and Homogeneity of Barrier Discharges in the Presence of Glass Dielectric, IEEE Transactions on Plasma Science, 2018, Vol. 46: p-p 3493 - 3498.
5. Gnapowski E., Gnapowski S., Pytka J., The impact of dielectrics on the electricalcapacity, concentration, efficiency ozonegeneration for the plasma reactor with meshelectrodes, Plasma Science and Technology, Vol. 20, Nr 8, p-p 1-7
6. Seraudie A., Vermeersch O., and Arnal D., "DBD Plasma actua-tor effect on a 2D model laminar boundary layer. Transition delay under ionic wind effect.", 29th AIAA Applied Aerodynamics Conference, Fluid Dynamics and Co-located Conferences.
7. Seraudie A., Aubert E., Naudé N., and Cambronne J., "Effect of Plasma Actuators on a Flat Plate Laminar Boundary Layer in Subsonic Conditions", 3rd AIAA Flow Control Conference, Fluid Dynamics and Co-located Conferences.
Published
2018-12-21
Issue
Section
Efektywność transportu/Transport efficiency
Copyright (c) 2018 Autobusy – Technika, Eksploatacja, Systemy Transportowe
This work is licensed under a Creative Commons Attribution 4.0 International License.
