Recent progress in flapping wing aerodynamics and aeroelasticity
Micro air vehicles (MAVs) have the potential to revolutionize our sensing and information
gathering capabilities in areas such as environmental monitoring and homeland security …
gathering capabilities in areas such as environmental monitoring and homeland security …
Reduced-order nonlinear unsteady aerodynamic modeling using a surrogate-based recurrence framework
B Glaz, L Liu, PP Friedmann - AIAA journal, 2010 - arc.aiaa.org
UNSTEADY aerodynamic models are critical components in computational aeroelastic
response and stability analyses. In addition to the time-history effects associated with …
response and stability analyses. In addition to the time-history effects associated with …
Low-Reynolds-number aerodynamics of a flapping rigid flat plate
Two-and three-dimensional low-aspect-ratio (AR 4) hovering airfoil/wing aerodynamics at a
low Reynolds number (Re 100) are numerically investigated. Regarding fluid physics, in …
low Reynolds number (Re 100) are numerically investigated. Regarding fluid physics, in …
ADVANCES AND PROSPECTS OF THE REDUCED ORDER\\MODEL FOR UNSTEADY FLOW AND ITS APPLICATION
G Chen, Y Li - 力学进展, 2011 - lxjz.cstam.org.cn
With the development of the large scale numerical simulation, computational fluid dynamics
and computational solid mechanics couplesimulation becomes the powerful accurate tool in …
and computational solid mechanics couplesimulation becomes the powerful accurate tool in …
[PDF][PDF] 非定常流场降阶模型及其应用研究进展与展望
陈刚， 李跃明 - 力学进展, 2011 - lxjz.cstam.org.cn
非定常流场降阶模型及其应用研究进展与展望 Page 1 第41 卷第6 期 力学进展 Vol. 41 No. 6
2011 年11 月25 日 ADVANCES IN MECHANICS Nov. 25, 2011 非定常流场降阶模型及其应用 …
2011 年11 月25 日 ADVANCES IN MECHANICS Nov. 25, 2011 非定常流场降阶模型及其应用 …
Fluid dynamics of pitching and plunging airfoils of Reynolds number between 1× 10^ 4 and 6× 10^ 4
C Kang, Y Baik, L Bernal, M Ol, W Shyy - 47th AIAA aerospace …, 2009 - arc.aiaa.org
I. Introduction he unsteady aerodynamics of biological flyers has been the subject of
numerous investigations by biologists and aerodynamicists. The recent monograph by Shyy …
numerous investigations by biologists and aerodynamicists. The recent monograph by Shyy …
Experimental investigation of pitching and plunging airfoils at Reynolds number between 1x10^ 4 and 6x10^ 4
YS Baik, J Rausch, L Bernal, M Ol - 39th AIAA fluid dynamics …, 2009 - arc.aiaa.org
This paper presents the results of an experimental investigation on the aerodynamics of
pitching and plunging airfoils. The research is motivated by recent interests on the …
pitching and plunging airfoils. The research is motivated by recent interests on the …
Effects of asymmetric stroke deviation on the aerodynamic performance of flapping wing
F Hu, Y Wang, D Li, X Liu - Proceedings of the Institution of …, 2023 - journals.sagepub.com
The kinematics of insect flapping flight are complex and asymmetric, which are contributed
to their superior flying capabilities, and the design of novel flapping micro air vehicles can …
to their superior flying capabilities, and the design of novel flapping micro air vehicles can …
Effects of stroke deviation on hovering aerodynamic performance of flapping wings
F Hu, X Liu - Physics of Fluids, 2019 - pubs.aip.org
In this paper, the typical normal-hovering mode with different surging motions is numerically
simulated by solving two-dimensional unsteady Navier-Stokes equations with the aim of …
simulated by solving two-dimensional unsteady Navier-Stokes equations with the aim of …
Optimization of flexible flapping-wing kinematics in hover
Hover-capable flapping-wing micro air vehicles are well suited for missions in confined
spaces. The best design practices for flapping wings and their kinematics are largely …
spaces. The best design practices for flapping wings and their kinematics are largely …