FIELD: aviation.
SUBSTANCE: aircraft of the aerodynamic design of the flying wing contains a wing of a thick profile designed for flight, having longitudinal and transverse axes, forming a configuration for flying at a subsonic speed and a configuration for flying at a hypersonic speed, engines and controls. The wing is made with the ability to fly at a subsonic speed in the direction of the transverse axis of the wing and with the ability to fly at a hypersonic speed in the direction of the longitudinal axis of the wing. The wing is made with the possibility of reducing the relative thickness of the profile and radii of curvature of the edges of the wing, lengthening the wing, increasing the sweep along the leading edges and narrowing the wing.
EFFECT: invention is aimed at expanding the arsenal of technical means.
8 cl, 4 dwg
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Authors
Dates
2021-03-15—Published
2019-07-05—Filed