Experimental study of the aerodynamics of a wing with various configurations of wingtip triangular extension
| Autor: | Gueraiche Djahid, S. A. Popov, A. V. Kuznetsov |
|---|---|
| Rok vydání: | 2016 |
| Předmět: |
0209 industrial biotechnology
Leading edge Engineering Wing business.industry Aerospace Engineering Wing configuration 02 engineering and technology Structural engineering Aerodynamics Vortex generator 020303 mechanical engineering & transports 020901 industrial engineering & automation Washout (aeronautics) 0203 mechanical engineering Wingtip vortices Wingtip device Aerospace engineering business |
| Zdroj: | Russian Aeronautics (Iz VUZ). 59:376-380 |
| ISSN: | 1934-7901 1068-7998 |
| DOI: | 10.3103/s1068799816030132 |
| Popis: | In this paper, we discuss the main ways of improving the aircraft aerodynamics. The results of a physical experiment are presented that is aimed to verify the theoretical results obtained earlier on the possible improvement in a seaplane wing model lift-to-drag ratio, by using a deflectable triangular extension along the wing leading edge near the wingtip. We confirm the slight effectiveness of using the wingtip leading edge triangular extensions on the nature of flow around the wing. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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