FIELD: aviation industry.
SUBSTANCE: fuselage nose is made in form of cone in front of which vortex generator is installed. Longitudinal plane of symmetry of vortex generator coincides with longitudinal plane of symmetry of flying vehicle. Vortex generator is provided with trailing edges whose outer ends are located at a distance from cone surface.
EFFECT: enlarged operating range of angles of attack.
4 dwg
Title | Year | Author | Number |
---|---|---|---|
FLYING VEHICLE | 1983 |
|
SU1840516A1 |
FLYING VEHICLE | 1981 |
|
SU1840518A1 |
DEVICE FOR ENHANCING AIRCRAFT STALL AND SPIN CHARACTERISTICS (VERSIONS) | 2005 |
|
RU2297364C1 |
FLYING VEHICLE | 2000 |
|
RU2187444C2 |
AIRCRAFT WITH FORE HORIZONTAL PLANE | 2003 |
|
RU2243131C1 |
CONVERTIBLE VERTICAL TAKE-OFF AND LANDING AIRCRAFT (VERSIONS) | 2014 |
|
RU2550589C1 |
FLIGHT MEASURING AIR PARAMETERS SYSTEM | 2005 |
|
RU2290646C1 |
DRONE AIRCRAFT | 2010 |
|
RU2461494C2 |
TOWED AERIAL FALSE TARGET | 2001 |
|
RU2206049C1 |
HIGHLY MANEUVERABLE AIRCRAFT | 2017 |
|
RU2682700C2 |
Authors
Dates
2007-05-20—Published
1981-05-29—Filed