论文标题
倾斜热板上自然注射气流流的非boussinesq稳定性分析
Non-Boussinesq stability analysis of natural-convection gaseous flow on inclined hot plates
论文作者
论文摘要
众所周知,浮力驱动的边界层流在半侵入倾斜的热板上发育,在距前缘的有限距离处变得不稳定,其特征在于基于局部边界层厚度的grashof数字GR的临界值。所产生的不稳定性的性质取决于倾斜角$ ϕ $,该$从垂直方向测量。对于低于临界值的$ ϕ $的值$ ϕ_c $,不稳定性的特征是跨度行驶波的外观,而对于$ ϕ> ϕ_c $,分叉流的流程显示了类似Görtler的流式涡流。在先前的线性稳定性分析中采用的BousSinesQ近似值,当壁式温度比$θ_W$不接近统一时,对气体流有效。此处介绍了相应的非BoussinesQ分析,还考虑了不同运输特性温度的变化。时间稳定性分析(包括基本流量的非平行效应)用于确定中性稳定性的曲线,然后将其用于描述临界数量的临界数量及其相关波长度对倾斜角$ ϕ $的依赖性以及对两个不稳定模式的温度比率$θ_W$的依赖,从而为两种不稳定性模式提供了$θ__w的配置的定量信息。该分析特别提供了交叉倾斜角$ ϕ_c $在$θ_W$上的预测依赖性,这表明,对于$θ_W-1 \ sim 1 $ Spanwise行进波的气体流动,在一系列倾斜角$ 0 \ le ϕ \ le ϕ_c $中,主要是比这比besss的更大范围。
The buoyancy-driven boundary-layer flow that develops over a semi-infinite inclined hot plate is known to become unstable at a finite distance from the leading edge, characterized by a critical value of the Grashof number Gr based on the local boundary-layer thickness. The nature of the resulting instability depends on the inclination angle $ϕ$, measured from the vertical direction. For values of $ϕ$ below a critical value $ϕ_c$ the instability is characterized by the appearance of spanwise traveling waves, whereas for $ϕ>ϕ_c$ the bifurcated flow displays Görtler-like streamwise vortices. The Boussinesq approximation, employed in previous linear stability analyses, ceases to be valid for gaseous flow when the wall-to-ambient temperature ratio $Θ_w$ is not close to unity. The corresponding non-Boussinesq analysis is presented here, accounting also for the variation with temperature of the different transport properties. A temporal stability analysis including nonparallel effects of the base flow is used to determine curves of neutral stability, which are then employed to delineate the dependences of the critical Grashof number and of its associated wave length on the inclination angle $ϕ$ and on the temperature ratio $Θ_w$ for the two instability modes, giving quantitative information of interest for configurations with $Θ_w-1\sim 1$. The analysis provides in particular the predicted dependence of the crossover inclination angle $ϕ_c$ on $Θ_w$, indicating that for gaseous flow with $Θ_w-1\sim 1$ spanwise traveling waves are predominant over a range of inclination angles $0 \le ϕ\le ϕ_c$ that is significantly wider than that predicted in the Boussinesq approximation.