Email this article Experimental investigation of lift for a wing-in-ground effect aircraft model
- Authors: Nazarov D.V.1, Frolov V.A.1, Shakhov V.G.1
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Affiliations:
- Samara University
- Issue: Vol 59, No 2 (2016)
- Pages: 206-210
- Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journal-vniispk.ru/1068-7998/article/view/229661
- DOI: https://doi.org/10.3103/S1068799816020082
- ID: 229661
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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.
About the authors
D. V. Nazarov
Samara University
Author for correspondence.
Email: dvn69@mail.ru
Russian Federation, Moskovskoe shosse 34, Samara, 443086
V. A. Frolov
Samara University
Email: dvn69@mail.ru
Russian Federation, Moskovskoe shosse 34, Samara, 443086
V. G. Shakhov
Samara University
Email: dvn69@mail.ru
Russian Federation, Moskovskoe shosse 34, Samara, 443086
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