NUMERICAL ANALYSIS OF THE INFLUENCE OF THE ANGLE OF ATTACK ON A TURBULENT FLOW AROUND A THICK PROFILE WITH VORTEX CELLS AT HIGH REYNOLDS NUMBERS

S. A. Isaev; P. A. Baranov; N. A. Kudryavtsev; I. A. Pyshnyi; A. G. Sudakov

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NUMERICAL ANALYSIS OF THE INFLUENCE OF THE ANGLE OF ATTACK ON A TURBULENT FLOW AROUND A THICK PROFILE WITH VORTEX CELLS AT HIGH REYNOLDS NUMBERS

机译：攻角对高雷诺数涡旋细胞厚壁周围湍流流动影响的数值分析

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A numerical investigation of the influence of the angle of attack on a turbulent flow around a thick profile with vortex cells at high Reynolds numbers has been carried out using the multiblock approach to solution of steady-state two-dimensional Reynolds equations closed by means of Menter's zonal model of shear-stress transfer.

机译：使用多块方法对由Menter方程封闭的稳态二维雷诺方程进行求解，对攻角对具有高雷诺数的涡流单元的厚轮廓周围湍流的影响进行了数值研究。剪切应力传递区域模型。

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《Journal of engineering physics and thermophysics 》 |2003年第4期| 共11页
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S. A. Isaev; P. A. Baranov; N. A. Kudryavtsev; I. A. Pyshnyi; A. G. Sudakov;
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1. NUMERICAL ANALYSIS OF THE INFLUENCE OF THE ANGLE OF ATTACK ON A TURBULENT FLOW AROUND A THICK PROFILE WITH VORTEX CELLS AT HIGH REYNOLDS NUMBERS [J] . S. A. Isaev, P. A. Baranov, N. A. Kudryavtsev, Journal of engineering physics and thermophysics . 2003 ,第4期

机译：攻角对高雷诺数涡旋细胞厚壁周围湍流流动影响的数值分析
2. Numerical simulation and experiments on turbulent air flow around the semi-circular profile at zero angle of attack and moderate Reynolds number [J] . Isaev Sergey, Baranov Paul, Popov Igor, Computers & Fluids . 2019 ,第期

机译：湍流空气流动的数值模拟与实验在零迎角下半圆形曲线上的湍流和中度雷诺数
3. Numerical simulation of the influence of viscosity turbulent flow around a thick airfoil with vortex cells [J] . S. A. Isaev, Yu. S. Prigorodov, A. G. Sudakov, Journal of engineering physics and thermophysics . 2002 ,第6期

机译：涡旋细胞厚翼型围绕粘度湍流影响的数值模拟
4. NUMERICAL SIMULATION OF TURBULENT FLOW OVER OF SEMI-CYLINDRICAL PROFILE AT ZERO ANGLE OF ATTACK [C] . Alexander Shebelev, Andrey Gavrilov Heat and Mass Transfer in the System of Thermal Modes of Energy - Technical and Technological Equipment . 2016

机译：半圆柱轮廓湍流湍流在零迎角下的数值模拟
5. Experimental investigations of the vortex flow behind a circular cone at high angles of attack. [D] . Asghar, Asad. 1992

机译：高攻角下圆锥体后部涡流的实验研究。
6. Numerical investigation of the vortex-induced vibration of an elastically mounted circular cylinder at high Reynolds number (Re = 104) and low mass ratio using the RANS code [O] . Niaz Bahadur Khan, Zainah Ibrahim, Linh Tuan The Nguyen, -1

机译：使用RANS代码对高雷诺数（Re = 104）和低质量比的弹性安装圆柱体的涡激振动进行数值研究
7. Numerical simulation and experiments on turbulent air flow around the semi-circular profile at zero angle of attack and moderate Reynolds number [O] . Sergey Isaev, Paul Baranov, Igor Popov, 2019

机译：湍流空气流动的数值模拟与实验在零迎角下半圆形曲线上的湍流和中度雷诺数
8. Results of a Study of Mach Number and Reynolds Number Effects on the Lee Side Vortex Flow Field Characteristics of an Ogive-Cylinder-Frustum-Cylinder at Angles of Attack to 25 Degrees, Volume 1 [R] . Foley, J. E. 1972

机译：马赫数和雷诺数对攻击角度为25度的Ogive-Cylinder-Frustum-Cylinder的李侧涡流场特性影响的研究结果，第1卷

NUMERICAL ANALYSIS OF THE INFLUENCE OF THE ANGLE OF ATTACK ON A TURBULENT FLOW AROUND A THICK PROFILE WITH VORTEX CELLS AT HIGH REYNOLDS NUMBERS

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