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Analysis of the Three-Dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow

机译：超音速和高超声速流动中尖锥上三维可压缩湍流边界层的分析

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An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.

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作者
Adams, J. C.;
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年度 1972
页码 p.1-92
总页数 92
原文格式 PDF
正文语种 eng
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关键词
Reentry vehicles ; Turbulent boundary layer ; Aerodynamic characteristics ; Numerical analysis ; Conical bodies ; Three-dimensional flow ; Mathematical models ; Angle of attack ; Experimental data ; Thermal properties ; Wind tunnel models ; Walls ; Flow fields;

机译：再入飞行器;湍流边界层;气动特性;数值分析;锥体;三维流动;数学模型;迎角;实验数据;热学性质;风洞模型;墙体;流场;

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专利

1. Inflow boundary condition for DNS of turbulent boundary layers on supersonic blunt cones [J] . DONG Ming, ZHOU Heng 应用数学和力学（英文版） . 2008,第008期

机译：超音速钝锥上湍流边界层DNS的流入边界条件
2. Inflow boundary condition for DNS of turbulent boundary layers on supersonic blunt cones [J] . 董明, 周恒应用数学和力学：英文版 . 2008,第008期

机译：超音速钝锥上湍流边界层DNS的流入边界条件
3. Experimental investigation of the influence of the passive porous coating on laminar-turbulent transition of the hypersonic boundary layer of the sharp cone at angles of attack [J] . Sergey Morozov, Sergey Lukashevich, Alexander Shiplyuk MATEC Web of Conferences . 2017,第1期

机译：被动多孔涂层对尖锐锥形边界层层状湍流转变的实验研究
4. INVESTIGATION OF BOUNDARY LAYER TRANSITION IN THREE-DIMENSIONAL SUPERSONIC FLOW OVER SHARP CONE [C] . Kozlovskiy V.A., Zemlyanskiy B.A., Kudryavtsev V.V., Proceedings of the 7th European symposium on aerothermodynamics. . 2011

机译：尖锥上三维超音速流动的边界层过渡研究
5. Investigation of Laser Discharge in a Supersonic Flow and Shock Wave Laminar Boundary Layer Interaction in a Hypersonic Flow [D] . Mortazavi Ravari, Mahsaalsadat. 2018

机译：超音速流中激光放电与高音速流中冲击波层流边界层相互作用的研究
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. Experimental investigation of the influence of the passive porous coating on laminar-turbulent transition of the hypersonic boundary layer of the sharp cone at angles of attack [O] . Sergey Morozov, Sergey Lukashevich, Alexander Shiplyuk 2017

机译：被动多孔涂层对尖锐锥形边界层层状湍流转变的实验研究

Analysis of the Three-Dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow

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