Aerodynamic performance study of propellers for Mars atmospheric environment

Abstract

In terms of flight conditions, the Martian atmospheric environment is undoubtedly much harsher than the Earth atmospheric environment, with extremely low air density, ultra-low Reynolds number, and raging Martian sandstorms, all of which have serious impacts on the design of Martian unmanned aerial vehicles (UAVs), especially for the design of the power system. The purpose of this paper is to study the impact of the Martian atmospheric environment on the aerodynamic performance of the propeller system. The computational fluid dynamics numerical simulation was used to study the impact of varying degrees of sand and dust accumulation on the aerodynamic performance of Martian propellers caused by Martian sandstorms and widespread dust. It was found that in the Martian atmospheric environment, the rough surface of propeller blades after sand and dust accumulation has better aerodynamic performance than the smooth surface, which is greatly different from the Earth environment; The aerodynamic characteristics of the propeller are tested in the simulated Martian atmosphere vacuum chamber environment, and the experiment has shown that the propeller has better aerodynamic performance under the condition of 8° angle of attack; under the condition of 8° angle of attack, the aerodynamic performance of the propeller is simulated by different Reynolds numbers and different Mach numbers, so as to obtain the influence of the Reynolds number and the Mach number on lift–drag characteristics under the Martian atmospheric environment, and then, the modified blead element theory suitable for the Martian atmospheric environment is derived, which provides a detailed reference for the accurate modeling of the Mars UAV. It has important guiding significance for the design of flight controller.