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强激波-附面层干扰下的气流动态畸变研究

THE INVESTIGATION OF DYNAMIC DISTORTIONS IN FLOWFIELD DOWNSTREAM OF STRONG SHOCK-BOUNDARY INTERACTION
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摘要 本文在一定附面层条件下,着重研究典型的强激波与紊流附面层干扰区下游扩压器出口的气流动态畸变,文中讨论了激波强度、扩压器壁面形状(直壁和曲壁)对动态畸变的影响.讨论了紊流度分布中四个峰值与相同截面上的总压沿高度分布的相互关系. In the condition of certain boundary layer,the dynamic flow distortion in a two-dimensional convergent-divergent duct at the interaction of typical strong shock to turbulent boundary layer is emphatically investigated in this paper.It is found experimentally that four turbulenlence peaks exist along the height of duct downstream of the interaction region,as well as that each peak corresponds respectively to the inflexion point of the Pitot pressure profile. The effects of shock strength and the duct geometry on the dynamic flow distortions are also discu-ssed.The power spectral density (PSD) and probability density function (PDF) of Pitot pressure signals at the typical condition of the turbulence profile are analyzed in detail.It is noticed that the pattern of PDF of the Pitot pressure signals in vortex sheet at intersection of λ-shock is similar to that of sine wave in Gaussian noise
作者 何中伟
机构地区 南京航空学院
出处 《推进技术》 EI CAS CSCD 北大核心 1989年第2期15-20,共6页 Journal of Propulsion Technology
关键词 流场畸度 激波干扰 进气道 频谱分析 Flow distortion,Shock wave interaction ,Inlet, Turbulence, Spectrum analysis
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参考文献1

  • 1何中伟.薄附面层的测量技术研究[J]航空学报,1982(02).

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