A Parametric study on the effects of winglet cant angle on wing aerodynamics and aeroacoustics

被引:1
作者
Vaezi, Erfan [1 ]
Madani, S. Amirreza S. [2 ]
Keshmiri, Amir [3 ]
机构
[1] Sharif Univ Technol, Dept Aerosp Engn, Azadi St, Tehran 111551639, Iran
[2] Delft Univ Technol, Fac Aerosp Engn, Kluyverweg 1, NL-2629 HS Delft, South Holland, Netherlands
[3] Univ Manchester, Sch Engn, Oxford Rd, Manchester M13 9PL, England
来源
SCIENTIFIC REPORTS | 2025年 / 15卷 / 01期
基金
英国工程与自然科学研究理事会;
关键词
Blended Winglet; Numerical Simulation; Cant Angle; Sensitivity Analysis; Aeroacoustic Performance; AIRCRAFT; PERFORMANCE; NOISE; OPTIMIZATION; GENERATION; REDUCTION; DESIGN; DRAG; FAN;
D O I
10.1038/s41598-024-84453-6
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
The use of winglet devices is an efficient technique for enhancing aerodynamic performance. This study investigates the effects of winglet cant angles on both the aerodynamics and aeroacoustics of a commercial wing, comparing them to other significant parameters using a parametric analysis. A Full Factorial Design method is employed to generate a matrix of experiments, facilitating a detailed exploration of flow physics, with lift-to-drag ratio (L/D) and the integral of Acoustic Power Level (APL) as the primary representatives of aerodynamic and acoustic performance, respectively. The RANS formulation, along with the \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$k{-}\epsilon$$\end{document} Realizable model and the Broadband Noise Source (BNS) model, are utilized to accurately simulate subsonic flows numerically. The study begins by examining the pressure coefficient (\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$C_p$$\end{document}) and APL distributions at various cant angles near the wingtip and root areas. The matrix of experiments is then analyzed to identify the most influential parameters based on the main effects of inputs and their two-way interactions. The results demonstrate that variations in winglet cant angle significantly alter the distribution of \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$C_p$$\end{document} and APL along the span, particularly near the wingtip, and that cant angle strongly impacts overall performance, at times even outweighing atmospheric parameters such as pressure and temperature.
引用
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页数:19
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