Numerical and experimental study of the aerodynamics of a civil-aircraft model at high angles of attack and during rotation

被引：0
|
作者：
Voevodin, A. V. [1 ]
Efremov, A. A. [1 ]
Soudakov, V. G. [1 ]
机构：
[1] Cent Aerohydrodynam Inst, Zhukovskii, Moscow Region, Russia
来源：
THERMOPHYSICS AND AEROMECHANICS | 2023年 / 30卷 / 01期
基金：
俄罗斯科学基金会;
关键词：
aerodynamics; civil aircraft; high angles of attack; rotation;
D O I：
10.1134/S0869864323010018
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A numerical and experimental study of the flow near a standard civil-aircraft model at high angles of attack in the range from 0 to 90 degrees and at subsonic velocities of the oncoming flow has been carried out. The experiments were performed in the T-105 wind tunnel of TsAGI. The calculations were carried out within the framework of solving the Reynolds-averaged Navier-Stokes equations. A comparison of the calculated and experimental integral characteristics showed a good agreement with an accuracy sufficient for practice. Physical features of the flow and their influence on the aerodynamic characteristics of a stationary model at high angles of attack, as well as in the regime of rotation of the model with a constant angular velocity, are revealed.
引用
收藏
页码：1 / 12
页数：12
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