e^(N)方法用于高超声速圆锥边界层转捩预测的可靠性  

Reliability of the e^(N)Method Applied to Hypersonic Blunt Cone Boundary Layers for Transition Prediction

作　　者：杨潇楠 苏彩虹 YANG Xiao-nan;SU Cai-hong(Laboratory for High-Speed Aerodynamics,Tianjin University,Tianjin 300072,China)

机构地区：[1]天津大学机械学院高速空气动力学研究室,天津300072

出　　处：《气体物理》2023年第2期44-55,共12页Physics of Gases

基　　金：国家自然科学基金(91952202,12072231)。

摘　　要：e^(N)方法基于扰动在边界层中线性演化过程中的幅值增长程度来预测转捩。以来流Mach数为6、不同壁面温度条件下不同钝度圆锥为研究对象,结合直接数值模拟和抛物化稳定性方程,从e^(N)方法是否能够准确描述扰动在上述边界层中线性增长的角度,分析了该方法预测转捩的可靠性。研究结果表明,在小钝度或高壁面温度情况下,扰动在向下游的演化过程中从第1模态转变为第2模态,基于线性稳定性理论的e^(N)方法变得不再可靠。壁面温度相同,头部钝度越大,e^(N)方法越可靠;同等钝度下,壁面温度越低,e^(N)方法越可靠。由于存在模态转换时,线性稳定性理论总是低估扰动的增长,因而对于给定的转捩判据N_(T)(可由某一工况实验标定给出),若钝度减小或壁面温度增加到一定程度,e^(N)方法给出的转捩位置比实际情况更靠后。重新标定转捩判据时,钝度越小,壁面温度越高,N_(T)的修正程度就越大。The e^(N)method predicts transition based on the level of the linear amplitude amplification of the disturbances in the boundary layer.Boundary layers over cones at Mach 6 were investigated with different nose bluntness and under different wall temperature conditions.Combined with direct numerical simulation(DNS)and parabolized stability equations(PSE),from the viewpoint whether the e^(N)method is able to accurately describe the amplification of the disturbances in the above boundary layers,its reliability for transition prediction was interrogated.Results show that in the cases of small bluntness or high wall temperature,the disturbances undergo the intermodal exchange from the first mode to the second mode when travelling downstream in the boundary layer,so that the e^(N)method based on linear stability theory becomes less reliable.Under the same wall temperature condition,as the nose bluntness increases,the e^(N)method is more reliable.For the same nose bluntness,as the wall temperature decreases,the e^(N)method is more reliable.Since linear stability theory always underestimates the amplification of the disturbances when there is an intermodal exchange,for the given transition criterion N_(T),which could be calibrated by a certain case,as the bluntness decreases or the wall temperature increases to some extent,the e^(N)method tends to produce a further downstream transition location than reality.To recalibrate the transition criterion,the smaller the nose bluntness or the higher the wall temperature,the larger the modification of N_(T)factor.

关 键 词：高超声速 边界层 线性稳定性理论 转捩预测 e^(N)方法 

分 类 号：O357.4[理学—流体力学]