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

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概要

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• 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.

著者

• Isogai Koji

  Nippon Bunri University

• Kamisawa Yuichi

  Nippon Bunri University

• Sato Hiroyuki

  Nippon Bunri University

関連論文

• Optimum Aeroelastic Design of Resonance Type Flapping Wing for Micro Air Vehicles
• Optimum Flapping Wing Motions of Dragonfly
• Optimum Aeroelastic Design of Resonance Type Flapping Wing for Micro Air Vehicle
• Resonance Type Flapping Wing for Micro Air Vehicle

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