Artificial insect wings of diverse morphology for flapping-wing micro air vehicles

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Artificial insect wings of diverse morphology for flapping-wing micro air vehicles.

The development of flapping-wing micro air vehicles (MAVs) demands a systematic exploration of the available design space to identify ways in which the unsteady mechanisms governing flapping-wing flight can best be utilized for producing optimal thrust or maneuverability. Mimicking the wing kinematics of biological flight requires examining the potential effects of wing morphology on flight per...

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Artificial insect wings of diverse morphology for flapping-wing MAVs

The development of flapping-wing micro air vehicles (MAVs) demands a systematic exploration of the available design space to identify ways in which the unsteady mechanisms governing flapping-wing flight can best be utilized for producing optimal thrust or maneuverability. Mimicking the wing kinematics of biological flight requires examining the potential effects of wing morphology on flight per...

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Control of Flapping-Wing Micro Air Vehicles

Most birds and many insects use periodic wing motion to propel themselves and maneuver. Most conventional flying machines are propelled by rotating machinery, achieve lift through rotating or fixed wings, and are controlled through the production of steady aerodynamic forces produced by rotors or movable wings. Many of the first powered flapping-wing micro air vehicles (MAVs) effectively replac...

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Computational Aeroelasticity Framework for Analyzing Flapping Wing Micro Air Vehicles

Due to their small size and flight regime, coupling of aerodynamics, structural dynamics, and flight dynamics is critical for Micro Aerial Vehicles. This paper presents a computational framework for simulating structural models of varied fidelity and a Navier-Stokes solver, aimed at simulating flapping and flexible wings. The structural model utilizes either (i) the in-house developed UM/NLABS,...

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ژورنال

عنوان ژورنال: Bioinspiration & Biomimetics

سال: 2009

ISSN: 1748-3182,1748-3190

DOI: 10.1088/1748-3182/4/3/036002