关键词: 乘波体, 稀薄气体效应, CFD模型, DSMC方法, 风洞实验

Abstract: Hypersonic vehicles in large airspace and wide speed range have become one of the current research hotspots, and waveriders have attracted significant attention due to their high lift-to-drag ratio and relatively simple shape. However, there is little research on the aerodynamic characteristics of waveriders under high-altitude rarefied conditions. Since the flow field encompasses multiple regimes ranging from continuum to rarefied, the accurate prediction of their aerodynamic characteristics remains a considerable challenge. This paper focuses on the rarefaction effect on aerodynamic characteristics of a waverider model, which is tested in the MARHy rarefied wind tunnel in France. Numerical simulations are performed using Direct Simulation Monte Carlo (DSMC) method, conventional Navier Stokes (NS) equations, and DSMC data improved Navier Stokes (DiNS) model. By comparing with experiment data, the computational accuracy of the different methods is evaluated. The aerodynamic characteristics of the waverider in the near-continuum regime are analyzed, with particular emphasis on the local rarefaction effects within the flow field and their influence on aerodynamic performance. Furthermore, the effects of Mach number and angle of attack are systematically investigated. The results show that under the experimental conditions of Mach 20 and Knudsen 0.01, the error in drag predicted by the conventional NS with slip boundary conditions reaches as high as 39.19% compared to experiment data. The DiNS model can reduce this relative error to 3.95% by correcting the linear constitutive relationship; For this waverider, skin friction contributes approximately 97.14% of the total drag. A pronounced shear nonequilibrium effect exists within the boundary layer, which invalidates the linear constitutive relations and causes the conventional NS equations to overpredict the skin friction. In addition, an increase in angle of attack leads to a significant increase in lift coefficient, a significant improvement in lift to drag ratio, and a more pronounced rarefaction effect; As the Mach number increases, the lift coefficient decreases significantly due to deviation from the design conditions, and the lift to drag ratio decreases significantly.

Key words: waverider, rarefaction effect, CFD model, DSMC method, wind tunnel test