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

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详细

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.

作者简介

D. Nazarov

Samara University

编辑信件的主要联系方式.
Email: dvn69@mail.ru
俄罗斯联邦, Moskovskoe shosse 34, Samara, 443086

V. Frolov

Samara University

Email: dvn69@mail.ru
俄罗斯联邦, Moskovskoe shosse 34, Samara, 443086

V. Shakhov

Samara University

Email: dvn69@mail.ru
俄罗斯联邦, Moskovskoe shosse 34, Samara, 443086

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