| 摘要 |
FIELD: aircraft engineering.SUBSTANCE: invention relates to aircraft engineering. Wing is made in form of variable cross-section tray converging from aircraft nose to tail. Wing consists of bearing frame, top and bottom skins, two lateral sections and two ailerons. Inside tray air flow divider is installed, on which four baffles are fixed, which lead part of air flow from tray through openings in side sections, thus creating additional negative pressure inside tray.EFFECT: invention is focused on increasing the lifting force.1 cl, 4 dwg |
