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Prediction of Laminar-to-Turbulent Boundary Layer Transition in Axial-Flow Turbomachinery

机译：轴流式透平机械中层流 - 湍流边界层转变的预测

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This paper first reviews current analytical studies regarding the laminar-to-turbulent boundary layer transition process, including relevant analysis of laminar separation, and then covers analytical and experimental studies concerning parametric effects on transition pertinent to axial-flow turbomachine blade rows. These include the effects of pressure gradient, freestream turbulence, surface roughness, heat transfer, and combined effects. Finally, the work of various authors who have established data correlations for transition on axial-flow turbomachine blade rows is evaluated. Their predictive equations and charts have been presented as a reference guide for determining the transition region on blades. Additionally, equations for calculating transitional boundary layer growth are presented. (Author)

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作者
Kluck, C. E.;
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年度 1981
页码 p.1-73
总页数 73
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Turbomachinery; Axial flow; Turbulence; Laminar flow; Predictions; Compressors; Boundary layer transition; Blades; Separation; Free stream; Pressure gradients; Heat transfer; Parametric analysis; Correlation techniques; Surface roughness; Equations; Charts; Computat;

机译：涡轮机械;轴向流动;湍流;层流;预测;压缩机;边界层过渡;叶片;分离;自由流;压力梯度;传热;参数分析;相关技术;表面粗糙度;方程;图表;计算;

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1. Improved Turbulence Prediction in Turbomachinery Flows and the Effect on Three-Dimensional Boundary Layer Transition [J] . Christoph Bode, Jens Friedrichs, Dominik Frieling, International Journal of Turbomachinery, Propulsion and Power . 2018,第3期

机译：改进的涡轮机械流动湍流预测及其对三维边界层过渡的影响
2. Laminar-to-turbulent transition in supersonic boundary layer: Effects of initial perturbation and wall heat transfer [J] . Sharma S., Shadloo M. S., Hadjadj A. Numerical Heat Transfer, Part A. Application: An International Journal of Computation and Methodology . 2018,第7a12期

机译：超声波边界层中的层状动荡过渡：初始扰动和壁传热的影响
3. Laminar-to-turbulent flow transition in directed injection through a perforated surface to a laminar boundary layer [J] . A. A. Klimov, S. A. Trdatyan Heat Transfer Research . 2000,第6a8期

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4. Direct Numerical Simulations of Laminar-to-Turbulent Transition in Laminar Separation Bubbles in Three-Dimensional Boundary-Layer [C] . Shirzad Hosseinverdi, Hermann F. Fasel AIAA aviation forum;AIAA fluid dynamics conference . 2016

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5. Prediction of transition for attached and separated shear layers in turbomachinery. [D] . Langtry, Robin Blair. 2003

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6. PNAS Plus: Transitional–turbulent spots and turbulent–turbulent spots in boundary layers [O] . Xiaohua Wu, Parviz Moin, James M. Wallace, 2017

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7. An algebraic model for prediction of bypass and separation-induced transition in turbomachinery boundary layers [O] . Kubacki Slawomir, Dick Erik 2016

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Prediction of Laminar-to-Turbulent Boundary Layer Transition in Axial-Flow Turbomachinery

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