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Effects of the injector geometry on a sonic jet into a supersonic crossflow
ISSN号:1674-7348
期刊名称:Science China Physics,Mechanics & Astonomy
时间:2013
页码:366-377
相关项目:激波和湍流旋涡分离共存的复杂流动的大涡和直接数值模拟
作者:
Wang, Guo-Lei|Chen, Li-Wei|Lu, Xi-Yun|
同期刊论文项目
激波和湍流旋涡分离共存的复杂流动的大涡和直接数值模拟
期刊论文 15
会议论文 9
同项目期刊论文
Statistical analysis of coherent vortical structures in a supersonic turbulent boundary layer
A consistent characteristic boundary condition for general fluid mixture and its implementation in a
Flow topology in compressible turbulent boundary layer
The Effect of Mach Number on Turbulence Behaviors in Compressible Boundary Layers
激波和湍流相互作用的数值模拟
Numerical investigation of a jet from a blunt body opposing a supersonic flow
Topological evolution in compressible turbulent boundary layer
Effect of wall temperature on hypersonic turbulent boundary layer
Effects of the jet-to-crossflow momentum ratio on a sonic jet into a supersonic crossflow
A numerical study of fluid injection and mixing under near-critical conditions
Interaction between strain and vorticity in compressible turbulent boundary layer
Characteristics of unsteady type IV shock/shock interaction
Large-eddy simulation of underexpanded supersonic swirling jets
Large eddy simulation of a vortex ring impacting a bump