Simulation of the flapping wing aerial vehicle using flexible multibody dynamics

被引：1
|
作者：
Choi, JaeWon [1 ]
Gong, DuHyun [1 ]
Lee, Junhee [1 ]
Kim, Chongam [2 ]
Shin, SangJoon [2 ]
机构：
[1] Seoul Natl Univ, Dept Aerosp Engn, Seoul, South Korea
[2] Seoul Natl Univ, Inst Adv Aerosp Technol, Seoul 08826, South Korea
来源：
INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES | 2021年 / 13卷
关键词：
Insect-type; flapping wing; finite-element-based flexible multibody dynamics; geometrically exact beam; trailing edge control; FLIGHT; MODEL;
D O I：
10.1177/17568293211043305
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
An insect-type flapping wing micro aerial vehicle offers high aerodynamic efficiency and maneuverability in confined spaces. The complicated aerodynamic/structural behavior of flapping wing micro aerial vehicle, however, causes difficulties regarding the dynamic control and parametric design. This paper develops a moderately accurate numerical framework taking into account the passive motion of the main wings. Finite-element-based multibody dynamics and two-dimensional unsteady aerodynamics are combined to simulate the hover of a flapping wing micro aerial vehicle. In addition, flexible and rigid wings are compared through numerical simulation considering the flexibility. In terms of the average thrust, numerical simulation by fluid-structure interaction shows good agreements against the experimental results within 5% discrepancy.
引用
收藏
页数：12
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