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Selected structural elements of the wing to increase the lift force

Autorzy
Treść / Zawartość
Identyfikatory
Warianty tytułu
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
Rocznik
Strony
764--767
Opis fizyczny
Bibliogr. 7 poz., fot., rys.
Twórcy
autor
  • 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.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-6b645418-116f-4d9b-bbce-096a008f271b
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