Numerical studies on steady interaction of low enthalpy hypersonic double wedge flows using different gas models
Numerical investigations and analyses are carried out particularly on the steady interactions of low enthalpy hypersonic 30-55-deg double wedge configuration at conditions similar to the experimental setup by Swantek & Austin. To achieve a steady solution, Re lower than those in the experiment are used. Three gas models, i.e., the perfect, equilibrium, and non-equilibrium gas models, are used to analyze the difference potentials that arise from the physical model. Grid convergence studies are first conducted at Ma=7 and Re=2.5e5/m. Subsequently, comprehensive numerical studies are carried out on the steady interactions and their evolution at Ma=7 and h0=2.1MJ/kg. Specifically: (a) The upper limits of Re are identified where the flows remain steady, and the corresponding interaction characteristics as well as differences in the three gas models are investigated. Notably, a quasi-normal shock wave is observed within the slip line passage in the case of the perfect gas model. (b) The flow characteristics of the three models, including the interaction pattern, geometric features of triple points, impingements, and separation zone, are studied and compared for Re=(4,3,2)e4/m. Differences primarily emerge between the results of the perfect gas model and the real gas model. Specifically, a transmitted shock reflecting above the separation zone is observed in the case of the perfect gas model. The effect of the gas model on temperature and specific heat ratio distributions, as well as the heat transfer and pressure coefficients over the wedge surface are investigated. The shock polar method is applied for comparison with computational results, while a 1D flow model is proposed to explain the occurrence of the quasi-normal shock wave. Finally, the effects of variations in Mach number and enthalpy are determined, by alternatively varying the two parameters around Ma=7 and h0=2.1MJ/kg at Re=4e4/m.