飞机尾涡流场参数的仿真计算方法研究综述
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摘要
作为缩减尾流间隔、提高运行效率的研究基础,尾涡流场的仿真计算技术是国内外民航空管研究领域的一个研究热点。在飞机尾涡流场的数值模拟方面,介绍了雷诺平均、大涡模拟和分离涡模拟方法在流场数值模拟方面的研究现状及存在问题;在尾涡流场参数的快速仿真计算方面,综述了典型计算模型的特点及存在的主要问题,包括CROW不稳定性、Greene消散模型、APA消散模型、TDAWP消散模型、D2P消散模型和三阶段消散模型等,分析了上述模型的精度与应用情况。最后对国内外研究现状进行了总结分析,提出了该领域未来的研究方向。
As the basis of the research on reducing wake vortex separations,numerical simulation and constructing of fast-models for simulating wake vortex have become the focus of many international ATM research institutes.In the research field of wake vortex numerical simulation,the formation,evaluation and decay of wake vortex are calculated based on RANS,LES or DES methods.These data can help to reveal the regulation of wake vortex,and can provide basic foundation for constructing wake vortex models.In the field of fast simulation of wake vortex,Some organizations have done many theoretical researches on the formation and dissipation of wake vortex,attempting to deduce the behavioural characteristics of wake vortex by establishing complex mathematical models,including CROW instability,Greene model,APA model,TDAWP model,D2 P model and the three-phase decay model,etc.The research status quo is analyzed and the key works in the next phase are also provided.
As the basis of the research on reducing wake vortex separations,numerical simulation and constructing of fast-models for simulating wake vortex have become the focus of many international ATM research institutes.In the research field of wake vortex numerical simulation,the formation,evaluation and decay of wake vortex are calculated based on RANS,LES or DES methods.These data can help to reveal the regulation of wake vortex,and can provide basic foundation for constructing wake vortex models.In the field of fast simulation of wake vortex,Some organizations have done many theoretical researches on the formation and dissipation of wake vortex,attempting to deduce the behavioural characteristics of wake vortex by establishing complex mathematical models,including CROW instability,Greene model,APA model,TDAWP model,D2 P model and the three-phase decay model,etc.The research status quo is analyzed and the key works in the next phase are also provided.
引文
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[14]JOURNADE J.Numerical wake vortex characterization[C]//AIAA Applied Aerodynamics Conference.American:AIAA,2013.
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[17]刘薇,宋国萍,褚双磊,等.基于Ansys Fluent的近场翼尖涡数值模拟与分析[J].飞行力学,2015,33(2):111-115.LIU W,SONG G P,CHU S L,et al.Numerical simulation and analysis of a wingtip vortex in the near field based on ansys fluent[J].Flight Dynamics,2015,33(2):111-115.(in Chinese)
[18]谷润平,宋国萍,刘薇.高雷诺数下二维翼型绕流气动特性数值分析[J].科学技术与工程,2014,14(21):162-166.GU R P,SONG G P,LIU W.Numerical analysis on aerodynamic characteristics of the flows with high Reynolds number around two-dimensional airfoil[J].Science Technology and Engineering,2014,14(21):162-166.(in Chinese)
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[22]JIANG L,CAI J,LIU C.Large-eddy simulation of wing tip vortex in the near field[J].International Journal of Computational Fluid Dynamics,2008,22(5):289-330.
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[25]MOKRY M.Numerical simulation of aircraft trailing vortices interacting with ambient shear or ground[J].Journal of Aircraft,2015,38(4):511-516.
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