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中国物理学会期刊

壁面质量引射气体性质对高超声速边界层稳定性的影响

CSTR: 32037.14.aps.74.20250385

Effects of wall-injected gas properties on hypersonic boundary layer instability

CSTR: 32037.14.aps.74.20250385
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  • 质量引射会对高超声速边界层稳定性和转捩产生显著影响. 本文采用多组分Navier-Stokes求解器, 计算了不同气体质量引射的流场, 在此基础上分析了质量引射对流动稳定性的影响, 区分了引射气体不同性质的作用. 研究表明, 质量引射排挤主流流体, 形成引射层, 令边界层变厚, 显著降低壁面摩阻和热流. 引射气体的黏性系数、相对分子质量及扩散作用主要影响边界层厚度, 而热传导系数和比热容则主要影响温度分布. 线性稳定性分析结果表明, 质量引射激发多个高阶模态失稳, 但第二模态仍起主导作用, 且质量引射减小第二模态失稳区域, 令扰动积分幅值显著减小, 进而抑制转捩. 引射气体性质的变化通过两条路径影响稳定性: 1)改变基本流剖面; 2)改变混合气体性质. 其中引射气体的输运系数(黏性、扩散)主要通过路径一改变失稳特征, 比热容主要通过路径二起作用, 相对分子质量则通过双路径共同作用.

     

    Active mass injection is an effective thermal protection technique that can significantly reduce wall heat flux. However, it inherently changes the stability characteristics of boundary layer, substantially affecting the laminar-to-turbulent transition process. Crucially, the underlying mechanisms of controlling how different injected gases regulate flow stability are still unclear. In order to systematically analyze the effects of different gas injections on flow stability, the gas-specific mass injection effects are investigated in this work by employing a multicomponent Navier-Stokes solver to compute flow fields with air, argon, and nitrogen injections. The influence of mass injection on flow stability is analyzed using linear stability theory, followed by distinguishing the different effects of various injectant properties. The result shows that mass injection can displace the freestream gas, forming an injection layer near the wall and increasing the thickness of the boundary layer. Herein, the properties of the main boundary layer are still similar to those of the original boundary layer, while the injection layer exhibits significantly reduced temperature and velocity gradients, resulting in decrease of wall heat flux and surface friction. Linear stability analysis reveals that when mass injection excites multiple higher-order instability modes, the second mode is still dominant. Notably, mass injection reduces the unstable region of the second mode and significantly lowers the integrated disturbance amplitude, thereby suppressing the transition. This stabilizing effect is more pronounced with lighter gases. The differences in injected gas properties are mainly reflected in the viscosity coefficient, thermal conductivity, relative molecular weight, and diffusivity. Among these, the boundary layer thickness is primarily affected by the viscosity coefficient, relative molecular weight, and diffusivity of the injected gas, while the temperature within the boundary layer decreases with the increase of thermal conductivity and specific heat capacity of the injected gas. The influence of injected gas properties on flow stability is manifested in two different ways: 1) Modification of basic flow profile and 2) change of mixed gas properties. Specifically, the transport coefficients (viscosity and diffusivity) of the injected gas mainly affect unstable characteristics through way 1), while the specific heat capacity mainly works through way 2). The relative molecular weight plays a combined role in the two ways.

     

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