Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion
نویسندگان
چکیده
منابع مشابه
Multibody Analysis of a Micro-aerial Vehicle Flapping Wing
Abstract. This paper discusses the use of multibody dynamics, augmented by the direct implementation of nonlinear finite element beams and significantly shells, to perform the coupled structural and fluid-dynamics analysis of flapping wing Micro-Aerial Vehicles. The implementation of the shell formulation in a free general-purpose multibody solver is described and validated. The solver, coupled...
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ژورنال
عنوان ژورنال: Journal of Applied Mathematics and Physics
سال: 2014
ISSN: 2327-4352,2327-4379
DOI: 10.4236/jamp.2014.212117