Optimum Aeroelastic Design of Resonance Type Flapping Wing for Micro Air Vehicles
نویسندگان
چکیده
منابع مشابه
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...
متن کاملConceptual design of flapping-wing micro air vehicles.
Traditional micro air vehicles (MAVs) are miniature versions of full-scale aircraft from which their design principles closely follow. The first step in aircraft design is the development of a conceptual design, where basic specifications and vehicle size are established. Conceptual design methods do not rely on specific knowledge of the propulsion system, vehicle layout and subsystems; these d...
متن کاملResonance Based Flapping Wing Micro Air Vehicle
Flapping wing micro air vehicles have many possible applications and have therefore been the subject of extensive research. The Atalanta project aims to develop a fully autonomous, 10 cm wingspan, flapping wing sensor platform. The structure is based on a fully compliant resonating structure with passive wing pitching. Several design improvements have taken place since the last report. Introduc...
متن کاملComputational 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,...
متن کاملA piezo‐driven flapping wing mechanism for micro air vehicles
2006). Flapping wing MAVs (FWMAVs) are a class of new conceptual MAVs that take design cues from flying insects in order to achieve a small size (<3–5 cm), high maneuverability and super remote ability (Yan et al. 2015). A FWMAV is expected to work in a variety of confined spaces such as urban canyons, caves, indoors, and jungles that large flying robots can’t be serviceable. To achieve such ta...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سال: 2010
ISSN: 0549-3811
DOI: 10.2322/tjsass.52.238