Numerical study on the flow characteristics of micro air vehicle wings at low Reynolds numbers

T Xiao, Z Li, S Deng, H Ang… - International Journal of …, 2016 - journals.sagepub.com
The aerodynamic characteristics around a micro air vehicle wing with an inverse-
Zimmerman configuration are numerically investigated by an in-house programmed solver …

Effect of skin flexibility on aerodynamic performance of flexible skin flapping wings for micro air vehicles

H Yusoff, MZ Abdullah, M Abdul Mujeebu… - Experimental …, 2015 - Springer
As part of the ongoing research on micro air vehicles, the present work focuses on the effect
of membrane flexibility on the aerodynamic performance of flexible latex flapping wings …

[引用][C] 单相机迎角测量中振动影响研究

孙岩, 姚海艳, 张征宇 - 航空学报, 2013

Experimental characterization of limit cycle oscillations in membrane wing micro air vehicles

JW Johnston, W Romberg, PJ Attar… - Journal of Aircraft, 2010 - arc.aiaa.org
The idea of using small-scale vehicles, often termed micro air vehicles, for various
surveillance applications has become increasingly popular in recent years. A micro air …

Study of Low Reynolds Number Aerodynamics for Low Aspect Ratio MAV Wing

TA Shams, SIA Shah, MA Ahmad - 2018 IEEE 21st International …, 2018 - ieeexplore.ieee.org
Aerodynamic research is primarily divided into two parts; fly higher, fly faster and fly low, fly
slow. This research is focused towards the later part of aerodynamic advancements, which …

Modal analysis of a flexible membrane wing of micro air vehicles

UK Chakravarty, R Albertani - Journal of Aircraft, 2011 - arc.aiaa.org
MICRO air vehicles (MAVs) are small (wing span on the order of 100 mm) and can fly at low
flight speeds (up to 15 m= s) in areas, where operate large aircraft are not feasible or …

[PDF][PDF] 风洞模型静弹性变形对气动力影响研究

孙岩, 张征宇, 邓小刚, 杨党国, 周桂宇 - 空气动力学学报, 2013 - kqdlxxb.xml-journal.net
介绍了一种基于模型变形视频测量系统和计算空气动力学研究静弹性变形对气动力影响的方法.
利用模型变形视频测量系统获取模型在气动载荷作用下的静弹性变形, 驱动模型表面网格运动 …

Analytical and finite element modal analysis of a hyperelastic membrane for micro air vehicle wings

UK Chakravarty - Journal of Vibration and Acoustics, 2013 - asmedigitalcollection.asme.org
Analytical and finite element models are developed for investigating the modal
characteristics of a hyperelastic rubber latex membrane for micro air vehicle wings …

[PDF][PDF] 柔性翼微型飞行器水平阵风响应特性实验研究

史志伟, 刘志强, 丁超 - 实验流体力学, 2010 - syltlx.com
设计研制了一种飞翼布局的柔性翼和刚性翼微型飞行器. 并在风洞中研究了两种微型飞行器在
定常风和水平阵风作用下的气动特性, 给出了柔性翼和刚性翼微型飞行器气动特性的差别 …

Vortex structure on twist-morphing micro air vehicle wings

NI Ismail, AH Zulkifli, RJ Talib… - … Journal of Micro Air …, 2016 - journals.sagepub.com
Vortex formation has numerous influences on the aerodynamic characteristics of fixed-wing
micro air vehicle wings. Despite the mature understanding of vortices on fixed-wing and …