Vertical take-off and landing tailstock type supersonic unmanned aerial vehicle
An unmanned aerial vehicle, vertical take-off and landing technology, applied in vertical take-off and landing aircraft, supersonic aircraft, aircraft and other directions, can solve the problems of difficult take-off and landing, high man-machine cost, and achieve the effect of high safety and reliability
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[0019] see figure 1 , the vertical take-off and landing tail seat type unmanned aerial vehicle of the present invention comprises fuselage 1, wing, engine 3 and vertical tail 4 four parts, and wing comprises inner wing 2 and outer wing 5.
[0020] The unmanned aerial vehicle adopts the aerodynamic layout of the double-swept single-wing, and the power adopts the engine 3 with thrust vectoring. All rooms are fusion designed.
[0021] The fuselage 1 has a slenderness ratio of 13; the design of the head side strip 0.3d or a shark head improves the asymmetrical nose vortex at a high angle of attack and suppresses the occurrence of side forces; the front fuselage: slenderness ratio: ln / d: 3, parabolic shape, shape curve: r / R=(x / ln)0.75, R is the radius of the bottom of the machine head 220mm, ln the length of the machine head is 0.8m; rear fuselage; tapered contraction; the middle part is used to place the fuel tank , flight control system, power supply and electrical system, etc...
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