利用涡流发生器和格尼襟翼组合增强倾转旋翼的升力

IF 1.1 4区工程技术 Q3 ENGINEERING, AEROSPACE

International Journal of Aerospace Engineering Pub Date : 2023-09-07 DOI:10.1155/2023/6646817

Hao Chen, Siliang Du, Zhong Chen

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引用次数: 0

摘要

近年来，利用涡发生器(VGs)和轮尼襟翼(GF)进行流动控制得到了广泛的关注，但它们各自独立。本研究的目的是对倾转旋翼的升力效应进行数值研究。采用reynolds -average Navier-Stokes (RANS)方程进行数值计算，采用Spalart-Allmaras单方程湍流模型进行求解。确定了两种控制装置在不同迎角下的单独和联合性能。结果表明，组合配置比单独使用任何一种装置都能提供更大的升力增强。与基准翼相比，两种装置的实施使失速攻角从10°增加到22°，最大升力系数提高了82.33%。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Lift Augmentation on a Tiltrotor Wing Using the Combination of Vortex Generators and Gurney’s Flap

Recently, flow control using vortex generators (VGs) and a Gurney flap (GF) has received considerable attention, but independently. The purpose of this study is to perform a numerical investigation into the lift augmentation effects of a tiltrotor wing with the combination of VGs and GF. The numerical results were obtained with the Reynolds-averaged Navier-Stokes (RANS) equations, and the turbulence was solved by the Spalart-Allmaras one-equation turbulence model. The separate and joint performances of these two control devices at different angles of attack are determined. It is shown that the combined configuration can provide greater lift augmentation than either device individually. Compared with the baseline wing, the implementation of both devices increases the stall angle of attack from 10° to 22°, and the maximum lift coefficient is improved by 82.33%.

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来源期刊

International Journal of Aerospace Engineering ENGINEERING, AEROSPACE-

CiteScore

2.70

自引率

7.10%

发文量

195

审稿时长

22 weeks

期刊介绍： International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.