FIELD: aeronautical engineering; lifting surfaces of various flying vehicles.
SUBSTANCE: proposed flying vehicle wing has additional aerodynamic surface in form of plate mounted on it. Plane is triangular in plan and its end edge is sharp and is parallel to wing axis of symmetry. Plate is located at distance from tip chord equal to 0.05-0.1 of wing span and its length is equal to 0.1-0.15 of wing chord at point of location of end edge of additional aerodynamic surface. Trailing edge of additional aerodynamic surface is rectilinear in form. Its upper surface is formed by extension of upper surface of wing and lower surface is smoothly conjugated with lower profile of wing tail section.
EFFECT: extended field of application; improved aerodynamic properties.
10 dwg
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Authors
Dates
2006-03-27—Published
2004-09-20—Filed