Отправить статью по E-mail Experimental investigation of lift for a wing-in-ground effect aircraft model
- Авторы: Nazarov D.1, Frolov V.1, Shakhov V.1
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Учреждения:
- Samara University
- Выпуск: Том 59, № 2 (2016)
- Страницы: 206-210
- Раздел: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/229661
- DOI: https://doi.org/10.3103/S1068799816020082
- ID: 229661
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Аннотация
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.
Об авторах
D. Nazarov
Samara University
Автор, ответственный за переписку.
Email: dvn69@mail.ru
Россия, Moskovskoe shosse 34, Samara, 443086
V. Frolov
Samara University
Email: dvn69@mail.ru
Россия, Moskovskoe shosse 34, Samara, 443086
V. Shakhov
Samara University
Email: dvn69@mail.ru
Россия, Moskovskoe shosse 34, Samara, 443086
