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5. Large eddy simulation of compressibility effects on supersonic boundary layer transition and turbule

Large eddy simulation of compressibility effects on supersonic boundary layer transition and turbule

来源 :7th International Conference on Fluid Mechamics(ICFM7)(第七届国际 | 被引量 : 0次 | 上传用户：zhangShunsheng

【摘 要】

：

The development of the near space super/hypersonic cruise aircraft has become one of the cutting-edges in aerospace technology in recent years.The flows are fre

【作 者】

：

S.Z.Wang J.M.Lei H.P.Zhen C.H.Lee 

【机 构】

：

SchoolofAerospaceEngineering,BeijingInstituteofTechnology,Beijing,100081,ChinaBeijingInstituteofSpac

【出 处】

：

7th International Conference on Fluid Mechamics(ICFM7)(第七届国际

【发表日期】

：

2015年5期

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论文部分内容阅读

The development of the near space super/hypersonic cruise aircraft has become one of the cutting-edges in aerospace technology in recent years.The flows are frequently transitional or turbulent in the aircraft boundary layer.

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