Further development of an algebraic intermittency model for separation-induced transition under elevated free-stream turbulence

S. Kubacki, D. Simoni, D. Lengani, M. Dellacasagrande, E. Dick
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Abstract

A constitutive law for the Reynolds stresses during boundary layer laminar-to-turbulent transition, constructed in previous work by elastic-net regression on an experimental data base, has been incorporated in an algebraic intermittency model. The objective is prediction improvement of transition in a separated layer under an elevated free-stream turbulence level. The modelling for such cases functions through additional production terms in the transport equations of turbulent kinetic energy and specific dissipation rate of a k-ω turbulence model. A sensor detects the front part of a separated layer and activates the production terms. These express the effect of Klebanoff streaks generated upstream of separation on the Kelvin-Helmholtz instability rolls in the separated part of the layer. By the Klebanoff streaks, the breakdown is faster and the speed of breakdown increases by the combined effects of a large adverse pressure gradient and an elevated free-stream turbulence level.
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自由湍流下分离诱导过渡代数间歇模型的进一步发展
先前在实验数据库上通过弹性网回归构建的边界层层流到湍流过渡期间的雷诺应力本构律已被纳入代数间歇模型中。目的是在自由流湍流水平升高的情况下,对分离层的转捩进行预测改进。这种情况下的建模是通过在k-ω湍流模型的湍流动能输运方程和比耗散率中附加产生项来实现的。传感器检测分离层的前部并激活生产条件。这表示分离上游产生的克里巴诺夫条纹对层分离部分的开尔文-亥姆霍兹不稳定辊的影响。在克利巴诺夫条纹中,击穿速度更快,并且由于较大的逆压梯度和较高的自由流湍流水平的综合作用,击穿速度加快。
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Turbulence measurements downstream of a combustor simulator designed for studies on the combustor-turbine interaction Development and research of efficiency of a new low-pressure turbine with one and a half exhaust based on forked two-tier blades Further development of an algebraic intermittency model for separation-induced transition under elevated free-stream turbulence
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