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Vortex structure simulation for supersonic mixing layers using nonlinear PSE method
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作者 Xin Guo Qiang Wang 《Theoretical & Applied Mechanics Letters》 2012年第3期53-56,共4页
The method of nonlinear parabolized stability equations(PSE) is applied in the simulation of vortex structures in compressible mixing layer.The spatially-evolving unstable waves,which dominate the vortex structure,a... The method of nonlinear parabolized stability equations(PSE) is applied in the simulation of vortex structures in compressible mixing layer.The spatially-evolving unstable waves,which dominate the vortex structure,are investigated through spatial marching method.The instantaneous flow field is obtained by adding the harmonic waves to basic flow.The results show that T-S waves do not keep growing exponentially as the linear evolution,the energy transfer to high order harmonic modes,and that finally all harmonic modes get saturated due to nonlinear interaction.The mean flow distortion induced by the nonlinear interaction between the harmonic modes and their conjugate harmonic ones,makes great change of the average flow and increases the thickness of mixing layer. PSE methods can well capture the two- and three-dimensional large scale nonlinear vortex structures in mixing layers such as vortex roll-up,vortex pairing,and A vortex. 展开更多
关键词 compressible mixing layer parabolized stability equations nonlinear stability vortex rollup vortex pairing A vortex
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三维机翼尾涡卷曲的数值模拟 被引量:4
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作者 蔡昊鹏 苏玉民 +1 位作者 李鑫 沈海龙 《大连海事大学学报》 CAS CSCD 北大核心 2009年第2期136-140,共5页
为使三维机翼尾涡卷曲更加真实,在计算诱导速度时引入衰减函数和有限半径涡核分别体现流体黏性作用下尾涡强度的衰减和尾涡扩散.应用面元法解析式计算奇点的诱导速度,在偶极附近区域用涡环代替偶极,利用尾涡面上的运动学条件来确定尾涡... 为使三维机翼尾涡卷曲更加真实,在计算诱导速度时引入衰减函数和有限半径涡核分别体现流体黏性作用下尾涡强度的衰减和尾涡扩散.应用面元法解析式计算奇点的诱导速度,在偶极附近区域用涡环代替偶极,利用尾涡面上的运动学条件来确定尾涡面的卷曲形状.数值模拟结果表明:涡核半径参数有一最佳值;考虑尾涡衰减可使卷曲更接近实验结果;采用曲线拟合方法确定衰减函数是可行的. 展开更多
关键词 机翼 尾涡卷曲 衰减函数 有限涡核
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