ABSTRACT Water air cross-medium vehicles have the advantage of cross-domain flight and have gradually become a research hotspot. However, existing technologies cannot provide better hydrodynamic performance while achieving efficient cross-medium vehicle efficiency. In this paper, A variant mechanism was designed based on the external characteristics of the submarine to achieve integrated of the rotor and the main hull of the aircraft, ensuring the underwater hydrodynamic performance of the aircraft. A tiltable tail rotor was designed to ensure stable flight of the aircraft in the airspace. To ensure the feasibility of the design, a computational fluid dynamics simulation was conducted on the hydrodynamic and aerodynamic performance of the spacecraft and rotor. The results show that the spacecraft can not only achieve stable navigation underwater and in the air, with good hydrodynamic and aerodynamic performance but also have advantages such as improving the efficiency of cross-medium vehicles and increasing their service.
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