FIELD: aviation industry.
SUBSTANCE: proposed flying vehicle has fuselage, wing with extensions and vortex generators with acute vertex, sweep-back sweep-forward edges. Vortex generators are installed along leading edge of extension.
EFFECT: enlarged operating range of angles of attack.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
FLYING VEHICLE | 1983 |
|
SU1840516A1 |
FLYING VEHICLE FUSELAGE NOSE | 1981 |
|
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RU2737816C1 |
Authors
Dates
2007-05-20—Published
1981-05-29—Filed