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本文引用的文献

1
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.
2
Analytical model for instantaneous lift and shape deformation of an insect-scale flapping wing in hover.悬停时昆虫尺度扑翼的瞬时升力和形状变形分析模型。
J R Soc Interface. 2014 Dec 6;11(101):20140933. doi: 10.1098/rsif.2014.0933.
3
Estimation of unsteady aerodynamics in the wake of a freely flying European starling (Sturnus vulgaris).自由飞翔的欧洲椋鸟(Sturnus vulgaris)尾迹中非定常空气动力学的估算。
PLoS One. 2013 Nov 22;8(11):e80086. doi: 10.1371/journal.pone.0080086. eCollection 2013.
4
Scaling law and enhancement of lift generation of an insect-size hovering flexible wing.昆虫大小的悬停柔性翼的升力产生的尺度律和增强。
J R Soc Interface. 2013 Jun 12;10(85):20130361. doi: 10.1098/rsif.2013.0361. Print 2013 Aug 6.
5
An aeroelastic instability provides a possible basis for the transition from gliding to flapping flight.气动弹性不稳定性为滑翔向扑翼飞行的转变提供了一个可能的基础。
J R Soc Interface. 2013 Jan 9;10(80):20120940. doi: 10.1098/rsif.2012.0940. Print 2013 Mar 6.
6
Rather than resonance, flapping wing flyers may play on aerodynamics to improve performance.扑翼飞行器可能不是利用谐振,而是利用空气动力学来提高性能。
Proc Natl Acad Sci U S A. 2011 Apr 12;108(15):5964-9. doi: 10.1073/pnas.1017910108. Epub 2011 Mar 28.
7
Influence of flexibility on the aerodynamic performance of a hovering wing.柔韧性对悬停机翼空气动力学性能的影响。
J Exp Biol. 2009 Jan;212(Pt 1):95-105. doi: 10.1242/jeb.016428.
8
Tuning of Strouhal number for high propulsive efficiency accurately predicts how wingbeat frequency and stroke amplitude relate and scale with size and flight speed in birds.为实现高推进效率而对斯特劳哈尔数进行调整,能准确预测鸟类的振翅频率和冲程幅度如何与体型及飞行速度相关联并随其变化。
Proc Biol Sci. 2004 Oct 7;271(1552):2071-6. doi: 10.1098/rspb.2004.2838.
9
The aerodynamics of insect flight.昆虫飞行的空气动力学
J Exp Biol. 2003 Dec;206(Pt 23):4191-208. doi: 10.1242/jeb.00663.
10
Flying and swimming animals cruise at a Strouhal number tuned for high power efficiency.飞行和游泳的动物以经过调整的斯特劳哈尔数巡航,以实现高功率效率。
Nature. 2003 Oct 16;425(6959):707-11. doi: 10.1038/nature02000.

展向柔性对前飞扑翼飞行器性能的影响。

Effects of spanwise flexibility on the performance of flapping flyers in forward flight.

机构信息

Department of Mechanical and Aerospace Engineering, University of Alabama in Huntsville, Huntsville, AL 35899, USA.

Department of Mechanical and Aerospace Engineering, University of Alabama in Huntsville, Huntsville, AL 35899, USA

出版信息

J R Soc Interface. 2017 Nov;14(136). doi: 10.1098/rsif.2017.0725.

DOI:10.1098/rsif.2017.0725
PMID:29167372
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC5721170/
Abstract

Flying animals possess flexible wings that deform during flight. The chordwise flexibility alters the wing shape, affecting the effective angle of attack and hence the surrounding aerodynamics. However, the effects of spanwise flexibility on the locomotion are inadequately understood. Here, we present a two-way coupled aeroelastic model of a plunging spanwise flexible wing. The aerodynamics is modelled with a two-dimensional, unsteady, incompressible potential flow model, evaluated at each spanwise location of the wing. The two-way coupling is realized by considering the transverse displacement as the effective plunge under the dynamic balance of wing inertia, elastic restoring force and aerodynamic force. The thrust is a result of the competition between the enhancement due to wing deformation and induced drag. The results for a purely plunging spanwise flexible wing agree well with experimental and high-fidelity numerical results from the literature. Our analysis suggests that the wing aspect ratio of the abstracted passerine and goose models corresponds to the optimal aeroelastic response, generating the highest thrust while minimizing the power required to flap the wings. At these optimal aspect ratios, the flapping frequency is near the first spanwise natural frequency of the wing, suggesting that these birds may benefit from the resonance to generate thrust.

摘要

飞行动物拥有灵活的翅膀,在飞行过程中会发生变形。翼弦方向的柔韧性会改变机翼形状,影响有效迎角,从而影响周围的空气动力学。然而,展向柔韧性对运动的影响尚未得到充分理解。在这里,我们提出了一种俯冲展向柔性机翼的双向耦合气动弹性模型。通过在机翼的每个展向位置评估二维、非定常、不可压缩位势流模型来模拟空气动力学。通过考虑横向位移作为在机翼惯性、弹性恢复力和空气动力的动态平衡下的有效下俯,实现了双向耦合。推力是机翼变形增强和诱导阻力之间竞争的结果。对于纯粹俯冲展向柔性机翼的结果与文献中的实验和高保真数值结果吻合较好。我们的分析表明,抽象的雀形目和鹅模型的机翼展弦比对应于最佳的气动弹性响应,在最小化翅膀拍打所需功率的同时产生最大的推力。在这些最佳展弦比下,拍打频率接近机翼的第一展向固有频率,这表明这些鸟类可能受益于共振来产生推力。