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LFC-16: world's first fighter maneuverability
发布时间:2010/12/4  阅读次数:527  字体大小: 【】 【】【

LFC-16: world's first fighter maneuverability

Cause the majority of the last air show enthusiasts and professionals pay attention to side duck layout fighter CY-1 (super-wing type I), in this air show by the name of LFC-16 re-appearance.

It is noteworthy that the aircraft used by the Chinese side of the duck pneumatic original layout, with the fixed side of the fin and other proprietary technologies; such as machine uses a series of new aerodynamic technology, including a machine body side duck pneumatic layout, With the dynamic side of the fin, controllable vortex and so on. Through the application of these techniques can improve aircraft handling and stability, or even to reach the level of propeller aircraft, while mobility will be greatly enhanced. Allegedly, the aircraft if successfully developed, will likely become the world's first fighter maneuverability. In addition the cost of the aircraft developed from the private venture capital funds, can be said that created a Chinese fighter in the history of precedent.

LFC-16 is quite unique with the body side, slightly lower than the canard plane of its location, width, great. Estimated effect is produced under a strong elevation in the large eddy current, eddy current coupling with the canard, the wing induce high lift. Help to improve the performance of the aircraft taking off and landing and hovering capabilities. Aircraft to improve handling and stability, depends on the active eddy current control and servo deflection with side fins, making the aircraft can not use fly-in and thrust vector control technology cases, can maintain stable high angle of attack and better handling. LFC-16 may be of real value or is it kept secret of the swirl control technology. This new type of aircraft will enhance the fighting capability is important.

LFC-16 Technical Data:

Length: 14.08 m

Wingspan: 8.32 m

Height: 5.03 m

Engine Thrust: 7000kg

Normal take-off weight: 8500kg

Take-off roll distance :300-400m

Landing roll :400-500 meters from the

Maximum speed: M1.6-1.8

The maximum instantaneous spiral angle: 30 degrees

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