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Developmant of an efficient numerical scheme for the computation of turbulent boundary layer flows over two-dimensional and axisymmetric bodies

机译：开发了一种有效的数值方案，用于计算二维和轴对称体上的湍流边界层流

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作者
Vatsa, V. N.; Goglia, G. L.;
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年度 1976
页码 1-47
总页数 47
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
NUMERICAL ANALYSIS; TURBULENT BOUNDARY LAYER; AXISYMMETRIC BODIES; TWO DIMENSIONAL BODIES; TWO DIMENSIONAL FLOW;

机译：数值分析;湍流边界层; aXIsYmmETRIC BODIEs;二维机构;二维流量;

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专利

1. Application of numerical schemes with singling out the boundary layer for the computation of turbulent flows using eddy-resolving approaches on unstructured grids [J] . Kozelkov A. S., Krutyakova O. L., Kurulin V. V., Computational mathematics and mathematical physics . 2017,第6期

机译：数值方案在非结构化网格上使用涡流方法计算湍流计算的边界层
2. A Numerical Scheme Based on an Immersed Boundary Method for Compressible Turbulent Flows with Shocks: Application to Two-Dimensional Flows around Cylinders [J] . Shun Takahashi, Taku Nonomura, Kota Fukuda Journal of applied mathematics . 2014,第Pta2期

机译：基于浸入边界法的可压缩湍流激波数值方案：在圆柱周围二维流中的应用
3. A Numerical Scheme Based on an Immersed Boundary Method for Compressible Turbulent Flows with Shocks: Application to Two-Dimensional Flows around Cylinders [J] . ShunTakahashi, TakuNonomura, KotaFukuda Journal of applied mathematics . 2014,第2期

机译：一种基于浸没边界法的压缩湍流流动与冲击的数值方案：应用于气缸周围的二维流动
4. Towards Stereoscopic PIV of Impinging Planar Shock/Turbulent Boundary Layer Interactions on an Axisymmetric Body [C] . Ramez M. Kiriakos, Arastou Pournadali Khamseh, Edward P. DeMauro AIAA SciTech Forum and Exposition . 2021

机译：朝向轴对称体撞击平面冲击/湍流边界层相互作用的立体PIV
5. BOUNDARY LAYER TRANSFER FOR NON-NEWTONIAN POWER-LAW FLUIDS OVER TWO-DIMENSIONAL OR AXISYMMETRICAL BODIES. [D] . KIM, HYUN WANG. 1980

机译：非牛顿动力法流体在二维或轴对称体上的边界层转移。
6. Boundary layer control by a fish: Unsteady laminar boundary layers of rainbow trout swimming in turbulent flows [O] . Kazutaka Yanase, Pentti Saarenrinne 2016

机译：鱼的边界层控制：虹鳟在湍流中游荡的不稳定层流边界层
7. Validation of High-Speed Turbulent Boundary Layer and Shock-Boundary Layer Interaction Computations with the OVERFLOW Code [O] . Lyrintizis A. S., Blaisdell G. A., Lillard R. P., 2006

机译：用OVERFLOW代码验证高速湍流边界层和冲击边界层相互作用计算
8. Numerical Computation of Shock Wave-Turbulent Boundary Layer Interaction in Transonic Flow over an Axisymmetric Curved Hill [R] . Kim, S. 1989

机译：轴对称曲线上跨声速冲击波 - 湍流边界层相互作用的数值计算

Developmant of an efficient numerical scheme for the computation of turbulent boundary layer flows over two-dimensional and axisymmetric bodies

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