CN CN121341396A
The invention provides a short-distance take-off and landing armor-wing aircraft depending on attack angle lift force, relates to the technical field of aircrafts, points out the essence that the attack angle lift force is from air acceleration, provides a flight theory of short-distance take-off and landing depending on the attack angle lift force, and systematically expounds the flight principle, trimming mechanism and control method of a flat-plate wing aircraft. The key points of aerodynamic layout design of the A-wing aircraft are summarized, aerodynamic layout planning and preliminary design calculation of short-distance take-off and landing flight depending on the attack angle lift force are provided, and accordingly the two-dimensional maneuvering characteristics and market application prospects of the A-wing aircraft are analyzed; the A-wing aircraft provided by the invention covers theoretical analysis, configuration design, parameter calculation, take-off and landing modes and flight control, and a complete technical scheme is formed.
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