Title :
Free-flight analysis of flapping flight during turning by fluid-structure interaction finite element analysis based on arbitrary Lagrangian-Eulerian method
Author :
Hamamoto, Masaki ; Ohta, Yoshiji ; Hara, Keita ; Hisada, Toshiaki
Author_Institution :
Devices Technol. Res. Labs., Sharp Corp., Tenri, Japan
fDate :
April 26-May 1, 2004
Abstract :
An insect´s flapping flight is an attractive method of transportation. It shows many useful flight modes such as maneuverable turning and stable hovering. In recent studies, experimental methods and numerical simulations have been successfully applied to solve the mechanism quantitatively. However, it is extremely difficult to accurately estimate the deformation of the wing caused by interaction with airflow. In prior studies, we analyzed this problem using a novel numerical simulation, fluid-structure interaction analysis, in order to represent this interactive behavior accurately, and achieved the quantitative evaluation of dragonfly hovering with flexible wings. As an advanced analysis, we added a solution of the interaction between the body and wings to the method, and realized free-flight simulation. Here, we demonstrate a sharp turn of 10 rad/s in a numerical simulation using a model based on an actual dragonfly.
Keywords :
aerodynamics; aerospace robotics; aerospace simulation; finite element analysis; mobile robots; numerical analysis; transportation; airflow; arbitrary Lagrangian-Eulerian method; dragonfly hovering; finite element analysis; flapping flight modes; flexible wings; fluid-structure interaction; free flight analysis; free flight simulation; maneuverable turning; numerical simulations; stable hovering; transportation; Aerodynamics; Analytical models; Equations; Finite element methods; Insects; Lagrangian functions; Motion analysis; Numerical simulation; Shape; Turning;
Conference_Titel :
Robotics and Automation, 2004. Proceedings. ICRA '04. 2004 IEEE International Conference on
Print_ISBN :
0-7803-8232-3
DOI :
10.1109/ROBOT.2004.1308763