Abstract 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.
Experimental investigation of lift for a wing-in-ground effect aircraft model
Russian Aeronautics (Iz VUZ) ; 59 , 2 ; 206-210
2016-04-01
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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