Optimum Aeroelastic Design of Resonance Type Flapping Wing for Micro Air Vehicles

被引：2
作者：
Isogai, Koji [1 ]
Kamisawa, Yuichi [1 ]
Sato, Hiroyuki [1 ]
机构：
[1] Nippon Bunri Univ, Oita, Japan
来源：
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 2010年 / 52卷 / 178期
关键词：
Flapping Wing; Resonance; Optimization; MAV; CFD; AERODYNAMICS;
D O I：
10.2322/tjsass.52.238
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The optimum aeroelastic design method for a resonance-type flapping wing for a Micro Air Vehicle (MAV) is presented. It uses Complex Method and 3D Navier-Stokes code to determine the optimum structural and aerodynamic parameters of a 2 DOF flapping wing system. The method is used to design a dragonfly-type MAV, and numerical simulation shows that the designed flapping wings can generate sufficient lift to sustain the weight and sufficient thrust to overcome the body drag.
引用
收藏
页码：238 / 245
页数：8
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