Мақаланы E-mail арқылы жіберу Experimental investigation of lift for a wing-in-ground effect aircraft model
- Авторлар: Nazarov D.1, Frolov V.1, Shakhov V.1
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Мекемелер:
- Samara University
- Шығарылым: Том 59, № 2 (2016)
- Беттер: 206-210
- Бөлім: 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
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
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.
Авторлар туралы
D. Nazarov
Samara University
Хат алмасуға жауапты Автор.
Email: dvn69@mail.ru
Ресей, Moskovskoe shosse 34, Samara, 443086
V. Frolov
Samara University
Email: dvn69@mail.ru
Ресей, Moskovskoe shosse 34, Samara, 443086
V. Shakhov
Samara University
Email: dvn69@mail.ru
Ресей, Moskovskoe shosse 34, Samara, 443086
