Experimental investigation of lift for a wing-in-ground effect aircraft model

Experimental investigation of lift for a wing-in-ground effect aircraft model

The aim of the investigation is to develop a technique of recalculating the lift as a function of the angle of attack at different reference points of the aircraft model height over the ground surface. A technique for evaluating the lift of the aircraft model close to the ground surface is proposed.

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Veröffentlicht in:Russian aeronautics 2016-04, Vol.59 (2), p.206-210
Hauptverfasser: Nazarov, D. V., Frolov, V. A., Shakhov, V. G.
Format: Artikel
Sprache:eng
Schlagworte:
Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
Automotive Engineering
Engineering
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Beschreibung
Zusammenfassung:The aim of the investigation is to develop a technique of recalculating the lift as a function of the angle of attack at different reference points of the aircraft model height over the ground surface. A technique for evaluating the lift of the aircraft model close to the ground surface is proposed.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799816020082