FIELD: aeronautical engineering.
SUBSTANCE: proposed flying vehicle has fuselage, wing with extensions-vortex generators with swept-forward and swept-back edges and additional vortex generator mounted in nose section of fuselage and high-lift devices for wing leading edge.
EFFECT: extended range of angles of attack.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
FLYING VEHICLE | 1981 |
|
SU1840518A1 |
FLYING VEHICLE FUSELAGE NOSE | 1981 |
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RU2737816C1 |
Authors
Dates
2007-05-27—Published
1983-03-21—Filed