The invention provides an air vehicle adopting a double-pointed-cone fish tail type front edge aerodynamic layout. The air vehicle comprises a vehicle body and an engine. The vehicle body comprises head pointed cones, a transition section, air inlet channel pointed cones and a blended wing body. The two head pointed cones are adopted and symmetrically arranged on the two sides, so that the low-pressure area of the head of the air vehicle is effectively enlarged, the trim capability of the whole vehicle is improved while the lift force is increased, and the trim resistance of the whole vehicle is reduced; by designing the transition section in the gap between the head pointed cones and the blended wing body, the vortex core central position on the inner sides of the head pointed cones is controlled, unfavorable interference between vortexes is reduced, the air flow energy of the upper surface is supplemented at the same time, and the lift force is increased; the air inlet channel pointed cones are arranged in the middle of the transition section, and then the vortex lift force of the upper surface of the air vehicle and high-angle-of-attack air inlet efficiency are improved; besides, the shielding effect on an air inlet channel is achieved through the head pointed cones and the transition section, and the hidden performance is improved; by means of the design of a plane groove surface between an air inlet channel lip and a tail jet nozzle on the lower surface of the air vehicle, the purpose of increasing the lift force is achieved. By means of the aerodynamic layout scheme, the hidden performance, taking-off and landing performance, subsonic speed and transonic speed maneuvering characteristics, the supersonic cruise performance, the poststall maneuver performance and other indexes can be well considered.