Key Parameters of a Design for a Novel Reflux Subsonic Low-Density Dust Wind Tunnel

Abstract

The dust storm on the surface of Mars is a severe threat to Mars exploration missions. Taking adequate measures to avoid the impact of the harsh wind-blown dust environment is indispensable. Ground simulation of the Martian high-speed windblown dust environment is helpful for analysis of the environmental effects and evaluations of the suitability of the components and materials. In this paper, a novel reflux subsonic low-density dust wind tunnel is presented to simulate the high-speed windblown dust environment of the Martian atmosphere with a velocity of more than 100 m/s. The sand and dust are fed into the wind tunnel through the ejector assembly together with the compressed gas, resulting in high uniformity of particles in the test section. The construction design of the Mars wind tunnel is introduced. The key parameters, which are the nozzle parameters and the contraction curve, are discussed in detail. The convergent nozzle is most suitable for the ejector assembly. Moreover, the bicubic curve is selected as the contraction curve. The gas-particle two-phase computational fluid dynamic (CFD) simulations demonstrate the rationality of the wind tunnel design.

Numerical modeling of two‐phase flows in the presence of dynamic and thermal interactions

“…To prevent the impact of an adverse wind environment, Wu et al 25 presented a model of a high‐speed aerodynamic dust environment. For this purpose, a subsonic wind tunnel with a low‐density dust particle reflow, developed by the authors, was used.…”