Review of Selected Methods for Increasing the Aerodynamic Force of the Wing

• Autorzy: Gnapowski Ernest

Identyfikatory

DOI

10.12913/22998624/103858

• Języki publikacji: EN

Abstrakty

EN

The manuscript presents the methods of increasing the aerodynamic force of the airfoil, currently used in aviation, and the directions of further research development. Currently, several methods are known and used to increase the aerodynamic force of the airfoil. The most widespread ones include wing mechanization systems, among others, flaps and slats. The non-mechanical elements of the wing construction that enable to increase the carrying force are used as well, among others; wing cuffs, vortilons, vortex generator. Research is being carried out on the introduction of mechanical elements that increase the lift force (Continuous Trailing Edge Flap, Morphing Wing), as well as non-mechanical elements such as plasma actuators. The manuscript describes the selected non-mechanical and mechanical elements currently used to increase the lift and the directions for the development of further research on increasing the aerodynamic force.

Słowa kluczowe

EN

high-lift device; lift force; plasma actuator; DBD discharge

PL

urządzenie wysokiego podnoszenia; siła podnoszenia; siłownik plazmowy; rozładowanie DBD

• Wydawca: Lublin University of Technology ; Polish Society of Ecological Engineering (PTIE), Branch of PTIE in Lublin
• Czasopismo: Advances in Science and Technology. Research Journal
• Rocznik: 2019
• Tom: Vol. 13, no 1
• Strony: 60--67
• Opis fizyczny: Bibliogr. 12 poz., fig.

Twórcy

autor

Gnapowski Ernest

• Department of Transport, University College of Enterprise and Administration, ul. Bursaki 12, 20-150 Lublin, Poland

Bibliografia

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• 2. 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, Vol. 46, 2018, 3493-3498.
• 3. Gnapowski S., Gnapowski E., Duda A., Inproving of the quality food for animals by pulsed power plasma discharge, Adv. Sci. Technol. Res. J., 9(27), 2015, 58-65.
• 4. Seraudie A., Aubert E., Naudé N., and Cambronne J., Effect of Plasma Actuators on a Flat Plate Laminar Boundary Layer in Subsonic Conditions, 2006, 3rd AIAA Flow Control Conference, Fluid Dynamics and Co-located Conferences.
• 5. Gnapowski E., Gnapowski S., Changes in the Power Discharge in a Plasma Reactor Using Porous Versus Solid Dielectric Barriers and Meshes Electrodes. IEEE Transactions on Plasma, 44(10), 2016, 2079-2083.
• 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, 2011, 29th AIAA Applied Aerodynamics Conference, Fluid Dynamics and Co-located Conferences.
• 7. 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, 20(8), 2018, 1-7, https://doi. org/10.1088/2058-6272/aac1b6
• 8. Ismail N.I., Zulkifli A.H., Abdullah M.Z., Basri M.H.M., Arif M., and Hamid A., Evolution of monoplane fixed wing micro air vehicle’s shape and design. Review. In: 2nd. International Conference on Arts, Social Sciences & Technology 2012.
• 9. Gnapowski E., Effect of Mesh Electrodes Geometry on the Ozone Concentration in the Presence of Micanite Dielectric. Advances in Science and Technology Research Journal, 12(4), 2018, 76–80, https://doi.org/10.12913/22998624/100340
• 10. Gudmundsson S., General Aviation Aircraft Design. Butterworth-Heinemann 2014.
• 11. Sofla A.Y.N., Meguid S.A., Tan K.T., and Yeo W.K., Shape morphing of aircraft wing: Status and challenges. Mater. Des., 31(3), 2010, 1284–1292.
• 12. Nhan T. Nguyen and Ezra A. Tal. A Multi-Objective Flight Control Approach for Performance Adaptive Aeroelastic Wing, 56th AIAA/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2015 AIAA (2015-1843).

Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).