| Title: | Подъёмная сила аэродинамического профиля с интерцептором |
| Other Titles: | Lift of the airfoil with spoiler |
| Authors: | Редькина, К.В. Фролов, В.А. |
| Issue Date: | 2012 |
| Publisher: | СГАУ |
| Citation: | Редькина, К. В. Подъёмная сила аэродинамического профиля с интерцептором = Lift of the airfoil with spoiler / К. В. Редькина, В. А. Фролов // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 333-334. |
| Abstract: | A model of a stationary vortex for the potential circulation flow around airfoil-spoiler combination has been proposed. The solution is obtained for the flow of incompressible ideal fluid. The Complex Variable Function Theory is applied. For the simulation of the recirculation area, a stationary vortex is used, the location of which is found by minimizing a velocity function. Dependence of the lift on the angle of attack, relative length of the spoiler and its angle of deflection is obtained. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/20411 |
| Appears in Collections: | Самолетостроение России. Проблемы и перспективы |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| 333-334.pdf | Основная статья | 1.71 MB | Adobe PDF | View/Open |
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