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Subisokinetic sampling characteristics of high speed aircraft inlets:A new CFD-based correlation considering inlet geometries

机译:高速飞机进气口的亚等速采样特性:考虑进气口几何形状的基于CFD的新关联

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Large spatial-scale atmospheric aerosol characterization is commonly accomplished from high-speed aircraft platforms using subisokinetic sampling.The aspiration efficiencies in these inlets are commonly determined from the empirical correlation of Belyaev and Levin [1974.Techniques for collection of representative aerosol samples.Journal of Aerosol Science,5,325-338](B&L),though the correlation was obtained from experiments under conditions very different from those encountered during highspeed aircraft sampling.Aircraft inlets are generally thick-walled,often have a blunt-body downstream,operate at a large free-stream to sampling velocity ratio,and under conditions of low ambient pressures.The dependence of sampling characteristics on these parameters is studied using computational fluid dynamics(CFD)modeling.The CFD calculations show that the anisokinetic inlet sampling characteristics are strongly influenced by the operating conditions and sampler geometry,especially the presence of an aft blunt body.It is observed that these dependencies are not accurately captured by the existing correlations.The presence of even a moderately sized blunt-body aft of a sampling inlet can greatly influence the sampling characteristics of a straight tube inlet.A new correlation is derived based on the CFD simulation results,and this correlation is seen to greatly improve prediction of inlet sampling characteristics considering their geometries.
机译:大型空间尺度的大气气溶胶表征通常是通过高速飞机平台使用等速动力学采样来完成的。这些进气口的抽吸效率通常由Belyaev和Levin [1974.经验性气溶胶相关性确定。气溶胶科学[5,325-338](B&L),尽管相关性是从与高速飞机采样所遇到的条件非常不同的条件下进行的实验获得的。飞机进气口通常是厚壁的,下游通常具有钝体,可在较大的压力下工作自由流与采样速度之比,并且在低环境压力下。使用计算流体力学(CFD)模型研究了采样特性对这些参数的依赖性。CFD计算表明,进气口的非等速采样特性受到强烈影响。操作条件和采样器的几何形状,尤其是存在观察到这些相关性不能通过现有的相关关系准确地捕捉到,即使是中等大小的采样入口的钝体尾部的存在也会极大地影响直管入口的采样特性。基于CFD仿真结果推导了Δε,并且考虑到其几何形状,这种相关性可以极大地改善入口采样特征的预测。

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