Transition Flight Simulation of Flapping-Wing Micro-Aerial Vehicle Using Aerodynamic Database

The paper describes how to simulate the flight of a flapping-wing micro-aerial vehicle (MAV). It uses an aerodynamic database generated using three-dimensional Navier-Stokes code. The database is composed of the time mean aerodynamic forces and moments generated at various flapping wing motions in v...

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Veröffentlicht in:	TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2010, Vol.53(180), pp.138-146
Hauptverfasser:	ISOGAI, Koji, KAWABE, Hiroyasu
Format:	Artikel
Sprache:	eng
Schlagworte:	Flapping Wing Flight Simulation Resonance
Online-Zugang:	Volltext
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