Aerodynamic characteristics of airfoil with single plain flap for light airplane wing

机译：轻型飞机机翼的单平面襟翼翼型的气动特性

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A numerical study was performed on a NACA 23012 airfoil with a single plain flap to examine the aerodynamic coefficients at Reynolds number of 3×10, and to help for identifying the forces acting on a light airplane wing. Besides, in the paper the flow fields around the airfoil with single plain flap were shown. All calculations were made using a CFD code. For a turbulent model the Spalart-Allmaras method was chosen. Conclusions were made about the aerodynamic efficiency of the proposed configuration wing-single plain flap.

机译：对具有单个平襟翼的NACA 23012机翼进行了数值研究，以检查雷诺数为3×10时的空气动力学系数，并有助于识别作用在轻型飞机机翼上的力。此外，在本文中，还显示了具有单个平瓣的翼型周围的流场。所有计算均使用CFD代码进行。对于湍流模型，选择了Spalart-Allmaras方法。对所提出的构型机翼-单平面襟翼的空气动力学效率作出了结论。

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《International Conference on Military Technologies》|2015年|1-6|共6页
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Todorov Michael;
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CFD; Fluent; aerodynamic characteristics; airplane wing; single plain flap;

机译：CFD;流质;空气动力学特性;飞机机翼;单平面襟翼;

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专利

1. Study the Influence of a Gap between the Wing and Slotted Flap over the Aerodynamic Characteristics of Ultra-Light Aircraft Wing Airfoil [J] . Cvetelina Velkova, Michael Todorov, Guillaume Durand 机械工程与自动化：英文版 . 2015,第005期

机译：研究机翼和缝隙襟翼之间的间隙对超轻型飞机机翼翼型气动特性的影响
2. Numerical Investigation on the Aerodynamic Characteristics of a Forward Flight Flapping Airfoil with Nonsymmetrical Plunging Motion [J] . Zhang Xingwei, Zhou Chaoying Information Technology Journal . 2011,第4期

机译：非对称切入运动的前向扑翼翼型气动特性的数值研究
3. Numerical Investigation on the Aerodynamic Characteristics of a Forward Flight Flapping Airfoil with Nonsymmetrical Plunging Motion [J] . Zhang Xingwei, Zhou Chaoying Information Technology Journal . 2011,第4期

机译：非对称俯冲运动的前向扑翼翼型气动特性的数值研究
4. Aerodynamic characteristics of airfoil with single plain flap for light airplane wing [C] . Todorov Michael International Conference on Military Technologies . 2015

机译：轻型翼片翼型的翼型空气动力学特性
5. An investigation of the dynamic effects of flap deflection on the aerodynamic characteristics of an airplane wing using computational fluid dynamics [D] . Moerchel, Alexander M. 2006

机译：利用计算流体力学研究襟翼偏转对飞机机翼空气动力学特性的动态影响
6. Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle [O] . G. Q. Zhang, S. C. M. Yu -1

机译：拍打翼微型飞机通风设计的空气动力学特性
7. STUDY OF THE INFLUENCE OF A GAP BETWEEN THE WING AND SLOTTED FLAP ON THE AERODYNAMIC CHARACTERISTICS OF ULTRA-LIGHT AIRCRAFT WING AIRFOIL [O] . Cvetelina VELKOVA, Michael TODOROV 2015

机译：研究机翼与开槽襟翼之间间隙对超轻型飞机翼翼型空气动力学特性的影响
8. Measurements of aerodynamic characteristics at transonic speeds of an unswept and untapered NACA 65-009 airfoil model of aspect ratio 3 with 1/4-chord plain flap by the NACA wing-flow method [R] . Johnson, Harold I 1953

机译：用NaCa翼流法测量长宽比为3的非扫描和非锥度NaCa 65-009翼型模型的跨音速空气动力学特性与1/4弦平面襟翼

Aerodynamic characteristics of airfoil with single plain flap for light airplane wing

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