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

页数：12

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