• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利：CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法，用中文像聊天一样搜索，搜遍4000万医学文献。AI智能推荐，让科研检索更轻松。

立即免费搜索

文件翻译

保留排版，准确专业，支持PDF/Word/PPT等文件格式，支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述，25分钟生成高质量综述，智能提取关键信息，辅助科研写作。

立即免费体验

基于地面效应的仿生波纹和弯度翼型空气动力学效率的数值研究。

Numerical investigation on the aerodynamic efficiency of bio-inspired corrugated and cambered airfoils in ground effect.

机构信息

Aerospace Engineering Department, Amirkabir University of Technology, Tehran, Iran.

Department of Mechanical and Aerospace Engineering, Tarbiat Modares University, Tehran, Iran.

出版信息

Sci Rep. 2022 Nov 9;12(1):19117. doi: 10.1038/s41598-022-23590-2.

DOI:10.1038/s41598-022-23590-2
PMID:36351992
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC9646766/
Abstract

This research numerically investigates the flapping motion effect on the flow around two subsonic airfoils near a ground wall. Thus far, the aerodynamic efficiency of the dragonfly-inspired flapping airfoil has not been challenged by an asymmetric cambered airfoil considering the ground effect phenomenon, especially in the MAV flight range. The analysis is carried out on the basis of an unsteady Reynolds-averaged Navier-stokes (URANS) simulation, whereby the Transition SST turbulence model simulates the flow characteristics. Dragonfly-inspired and NACA4412 airfoils are selected in this research to assess the geometry effect on aerodynamic efficiency. Moreover, the impacts of Reynolds number (Re), Strouhal number (St), and average ground clearance of the flapping airfoil are investigated. The results indicate a direct relationship between the airfoil's aerodynamic performance ([Formula: see text]/[Formula: see text]) and the ground effect. The [Formula: see text]/[Formula: see text] increases by reducing the airfoil and ground distance, especially at [Formula: see text]. At [Formula: see text], by increasing the St from 0.2 to 0.6, the values of [Formula: see text]/[Formula: see text] decrease from 10.34 to 2.1 and 3.22 to 1.8 for NACA4412 and dragonfly airfoils, respectively. As a result, the [Formula: see text]/[Formula: see text] of the NACA4412 airfoil is better than that of the dragonfly airfoil, especially at low oscillation frequency. The efficiency difference between the two airfoils at St=0.6 is approximately 14%, indicating that the [Formula: see text]/[Formula: see text] difference decreases substantially with increasing frequency. For [Formula: see text], the results show the dragonfly airfoil to have better [Formula: see text]/[Formula: see text] in all frequencies than the NACA4412 airfoil.

摘要

本研究通过数值模拟的方式研究了近壁面条件下，两个亚声速翼型扑翼运动对绕流的影响。迄今为止，考虑到地面效应现象，还没有对具有非对称弯度翼型的蜻蜓启发式扑翼空气动力效率进行挑战，特别是在微型飞行器飞行范围内。本研究基于非定常雷诺平均纳维-斯托克斯（URANS）模拟进行分析，其中过渡 SST 湍流模型模拟了流动特性。本研究选择了蜻蜓启发式翼型和 NACA4412 翼型来评估几何形状对空气动力效率的影响。此外，还研究了雷诺数（Re）、斯特劳哈尔数（St）和扑翼空气动力平均离地间隙的影响。结果表明，翼型空气动力性能([Formula: see text]/[Formula: see text])与地面效应之间存在直接关系。随着翼型和地面距离的减小，[Formula: see text]/[Formula: see text]增加，特别是在[Formula: see text]。在[Formula: see text]时，通过将 St 从 0.2 增加到 0.6，NACA4412 翼型和蜻蜓翼型的[Formula: see text]/[Formula: see text]值分别从 10.34 减小到 2.1 和从 3.22 减小到 1.8。因此，NACA4412 翼型的[Formula: see text]/[Formula: see text]优于蜻蜓翼型，特别是在低振荡频率时。在 St=0.6 时，两种翼型的效率差异约为 14%，表明随着频率的增加，[Formula: see text]/[Formula: see text]的差异会显著减小。对于[Formula: see text]，结果表明在所有频率下，蜻蜓翼型的[Formula: see text]/[Formula: see text]都优于 NACA4412 翼型。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/6bbdb919f228/41598_2022_23590_Fig20_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/05844fb537c7/41598_2022_23590_Fig1_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/8708881eee3a/41598_2022_23590_Fig2_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/59be7975551f/41598_2022_23590_Fig3_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/d1d40fef8cbc/41598_2022_23590_Fig4_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/a1b009929295/41598_2022_23590_Fig5_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/c6f880187ef8/41598_2022_23590_Fig6_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/51d9e0762217/41598_2022_23590_Fig7_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/921e33fbbf6e/41598_2022_23590_Fig8_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/62d7aaaa5ea5/41598_2022_23590_Fig9_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/40bba125ee47/41598_2022_23590_Fig10_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/967222d4cd7f/41598_2022_23590_Fig11_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/3bfb1b5ec4fc/41598_2022_23590_Fig12_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/b6d40e070f3f/41598_2022_23590_Fig13_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/8c32e96b11a9/41598_2022_23590_Fig14_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/4fc0068b31f4/41598_2022_23590_Fig15_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/50ead74878e6/41598_2022_23590_Fig16_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/6448da2b828d/41598_2022_23590_Fig17_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/0defa83a2fd7/41598_2022_23590_Fig18_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/580a5401030c/41598_2022_23590_Fig19_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/6bbdb919f228/41598_2022_23590_Fig20_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/05844fb537c7/41598_2022_23590_Fig1_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/8708881eee3a/41598_2022_23590_Fig2_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/59be7975551f/41598_2022_23590_Fig3_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/d1d40fef8cbc/41598_2022_23590_Fig4_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/a1b009929295/41598_2022_23590_Fig5_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/c6f880187ef8/41598_2022_23590_Fig6_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/51d9e0762217/41598_2022_23590_Fig7_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/921e33fbbf6e/41598_2022_23590_Fig8_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/62d7aaaa5ea5/41598_2022_23590_Fig9_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/40bba125ee47/41598_2022_23590_Fig10_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/967222d4cd7f/41598_2022_23590_Fig11_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/3bfb1b5ec4fc/41598_2022_23590_Fig12_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/b6d40e070f3f/41598_2022_23590_Fig13_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/8c32e96b11a9/41598_2022_23590_Fig14_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/4fc0068b31f4/41598_2022_23590_Fig15_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/50ead74878e6/41598_2022_23590_Fig16_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/6448da2b828d/41598_2022_23590_Fig17_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/0defa83a2fd7/41598_2022_23590_Fig18_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/580a5401030c/41598_2022_23590_Fig19_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2838/9646766/6bbdb919f228/41598_2022_23590_Fig20_HTML.jpg

相似文献

1
Numerical investigation on the aerodynamic efficiency of bio-inspired corrugated and cambered airfoils in ground effect.基于地面效应的仿生波纹和弯度翼型空气动力学效率的数值研究。
Sci Rep. 2022 Nov 9;12(1):19117. doi: 10.1038/s41598-022-23590-2.
2
Enhancement of aerodynamic performance of a heaving airfoil using synthetic-jet based active flow control.基于合成射流的主动流动控制增强纵振翼型的空气动力性能。
Bioinspir Biomim. 2018 May 25;13(4):046005. doi: 10.1088/1748-3190/aabdb9.
3
Numerical investigation of low-noise airfoils inspired by the down coat of owls.受猫头鹰羽绒服启发的低噪声翼型的数值研究。
Bioinspir Biomim. 2018 Dec 7;14(1):016013. doi: 10.1088/1748-3190/aaf19c.
4
Parameter study of simplified dragonfly airfoil geometry at Reynolds number of 6000.在雷诺数为 6000 的情况下，对简化版蜻蜓翼型几何形状的参数研究。
J Theor Biol. 2010 Oct 21;266(4):691-702. doi: 10.1016/j.jtbi.2010.07.016. Epub 2010 Jul 29.
5
Theoretical study on two-dimensional aerodynamic characteristics of unsteady wings.非定常机翼二维气动特性的理论研究
J Theor Biol. 2005 May 7;234(1):67-78. doi: 10.1016/j.jtbi.2004.11.016. Epub 2005 Jan 4.
6
Optimal design of aeroacoustic airfoils with owl-inspired trailing-edge serrations.基于猫头鹰翼梢锯齿的翼型声学风洞优化设计
Bioinspir Biomim. 2021 Jul 15;16(5). doi: 10.1088/1748-3190/ac03bd.
7
Hovering efficiency comparison of rotary and flapping flight for rigid rectangular wings via dimensionless multi-objective optimization.通过无量纲多目标优化对刚性矩形翼的旋转和扑翼飞行的悬停效率进行比较。
Bioinspir Biomim. 2018 May 8;13(4):046002. doi: 10.1088/1748-3190/aab801.
8
Aerodynamic Effects of Time-Varying Corrugations on Dragonfly Wings in Flapping Flight.扑翼飞行中蜻蜓翅膀上随时间变化的波纹的空气动力学效应。
Biomimetics (Basel). 2024 Jul 17;9(7):433. doi: 10.3390/biomimetics9070433.
9
Effect of the shape of flapping airfoils on aerodynamic forces.扑翼机翼形状对气动力的影响。
Heliyon. 2024 Apr 15;10(8):e29561. doi: 10.1016/j.heliyon.2024.e29561. eCollection 2024 Apr 30.
10
Covert-inspired flaps for lift enhancement and stall mitigation.基于掩蔽理论设计的高升力襟翼及其失速缓解。
Bioinspir Biomim. 2021 Jun 22;16(4). doi: 10.1088/1748-3190/abf3b3.

引用本文的文献

1
Aerodynamic Characteristics of a Tandem Flapping Wing in Inclined Stroke Plane Hovering with Ground Effect.倾斜行程平面悬停且有地面效应时串列扑翼的空气动力学特性
Biomimetics (Basel). 2025 Mar 30;10(4):212. doi: 10.3390/biomimetics10040212.

本文引用的文献

1
Numerical modeling of dielectric barrier discharge actuators based on the properties of low-frequency plasmons.基于低频等离子体特性的介质阻挡放电致动器的数值模拟
Sci Rep. 2022 Jun 20;12(1):10378. doi: 10.1038/s41598-022-14370-z.
2
Combined effects of body posture and three-dimensional wing shape enable efficient gliding in flying lizards.身体姿势和三维翅膀形状的综合效应使飞行蜥蜴能够高效滑行。
Sci Rep. 2022 Feb 2;12(1):1793. doi: 10.1038/s41598-022-05739-1.
3
Scaling trends of bird's alular feathers in connection to leading-edge vortex flow over hand-wing.
手翼前缘涡旋流中鸟翼翼尖羽毛的缩放趋势。
Sci Rep. 2020 May 13;10(1):7905. doi: 10.1038/s41598-020-63181-7.
4
Experimental and Numerical Investigation on Dragonfly Wing and Body Motion during Voluntary Take-off.蜻蜓在自主起飞过程中翅膀和身体运动的实验和数值研究。
Sci Rep. 2018 Jan 17;8(1):1011. doi: 10.1038/s41598-018-19237-w.
5
Rolling and pitching oscillating foil propulsion in ground effect.地面效应中滚动和俯仰摆动翼推进。
Bioinspir Biomim. 2017 Nov 27;13(1):016003. doi: 10.1088/1748-3190/aa8a12.
6
Aerodynamics, sensing and control of insect-scale flapping-wing flight.昆虫尺度扑翼飞行的空气动力学、传感与控制
Proc Math Phys Eng Sci. 2016 Feb;472(2186):20150712. doi: 10.1098/rspa.2015.0712.
7
Aerodynamic performance of the feathered dinosaur Microraptor and the evolution of feathered flight.有羽恐龙小盗龙的空气动力学性能与羽毛飞行的演化。
Nat Commun. 2013;4:2489. doi: 10.1038/ncomms3489.
8
A computational study of the aerodynamic performance of a dragonfly wing section in gliding flight.蜻蜓翅膀截面在滑翔飞行中空气动力学性能的计算研究。
Bioinspir Biomim. 2008 Jun;3(2):026004. doi: 10.1088/1748-3182/3/2/026004. Epub 2008 May 23.
9
Aerodynamic characteristics of dragonfly wing sections compared with technical aerofoils.蜻蜓翼型与技术翼型的空气动力学特性比较。
J Exp Biol. 2000 Oct;203(Pt 20):3125-35. doi: 10.1242/jeb.203.20.3125.
10
Aerodynamic characteristics of the wings and body of a dragonfly.蜻蜓翅膀和身体的空气动力学特征。
J Exp Biol. 1996;199(Pt 2):281-94. doi: 10.1242/jeb.199.2.281.