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

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概要

• 論文の詳細を見る

• 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.

• 社団法人 日本航空宇宙学会の論文
• 2010-02-04

著者

• ISOGAI Koji

  Department of Aerospace Engineering, Nippon Bunri University

• Isogai Koji

  Nippon Bunri University

• Kamisawa Yuichi

  Nippon Bunri University

• Sato Hiroyuki

  Nippon Bunri University

• Isogai Koji

  Nippon Bunri Univ.

• Kamisawa Yuichi

  Nippon Bunri Univ.

関連論文

• Optimum Aeroelastic Design of Resonance Type Flapping Wing for Micro Air Vehicles
• Development of Bird-like Micro Aerial Vehicle with Flapping and Feathering Wing Motions
• Optimum Flapping Wing Motions of Dragonfly
• Transition Flight Simulation of Flapping-Wing Micro-Aerial Vehicle Using Aerodynamic Database
• Optimum Aeroelastic Design of Resonance Type Flapping Wing for Micro Air Vehicle
• Resonance Type Flapping Wing for Micro Air Vehicle
• Aerodynamic Study and Mechanization Concepts for Flapping-Wing Micro Aerial Vehicles
• Shape Optimization of Fish Tail Propulsion with Hydro-Elastic Effects

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