Selected structural elements of the wing to increase the lift force

• Autorzy: Gnapowski E.

Identyfikatory

DOI

10.24136/atest.2018.494

• Języki publikacji: EN

Abstrakty

EN

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.

Słowa kluczowe

EN

aerodynamic; high-lift device; plasma actuator DBD

• Wydawca: Instytut Naukowo-Wydawniczy "SPATIUM". sp. z o.o.
• Czasopismo: Autobusy : technika, eksploatacja, systemy transportowe
• Rocznik: 2018
• Tom: R. 19, nr 12
• Strony: 764--767
• Opis fizyczny: Bibliogr. 7 poz., fot., rys.

Twórcy

autor

Gnapowski E.

• Department of Transport, University College of Enterprise and Administration, Lublin

Bibliografia

• 1. Crane, Dale: Dictionary of Aeronautical Terms, third edition, page 144. Aviation Supplies & Academics, 1997.
• 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 electrical capacity, concentration, efficiency ozonegeneration for the plasma reactor with mesh electrodes, Plasma Science and Technology, Vol. 20, Nr 8, p-p 1-7.
• 6. Seraudie A., Vermeersch O., and Arnal D., "DBD Plasma actuator 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.