Static Hysteresis of the Aerodynamic Characteristics of a Model Aircraft in the Landing Regime

被引：3
|
作者：
Voevodin, A. V. [1 ]
Soudakov, V. G. [1 ]
机构：
[1] Cent Aerohydrodynam Inst TsAGI, Ul Zhukovskogo 1, Zhukovskii 140180, Moscow Oblast, Russia
来源：
FLUID DYNAMICS | 2018年 / 53卷 / 04期
关键词：
static hysteresis; numerical modeling; aircraft; high-lift wing; landing regime;
D O I：
10.1134/S0015462818040122
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
Flow past a simplified model of the civil aircraft is numerically investigated in the landing regime. The numerical modeling is performed within the framework of the Reynolds equations. The aerodynamic characteristics of the model are studied. Regimes with the static hysteresis are found.
引用
收藏
页码：510 / 516
页数：7
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