Kinematic and Aerodynamic Investigation of the Butterfly in Forward Free Flight for the Butterfly-Inspired Flapping Wing Air Vehicle

نویسندگان

چکیده

To ensure the stability of flight, butterfly needs to flap its wings and simultaneously move main body achieve all kinds flying motion, such as taking off, hovering, or reverse flight. The high-speed camera is used record swing abdomen, movement wings, pitch angle for butterflies during their free flight; comprehensive biokinetic observations show that butterfly’s are coupled in various flight states. abdomen fore wing affect motion significantly. For theoretical analysis a three-dimensional multi-rigid model based on real dimension established, aerodynamic simulated analyzed via computational fluid dynamics methods obtain an optimal kinematic forward Moreover, formation development vortex structures also presented. detailed vortices dynamic behavior wing’s abdominal play key role reorienting correcting “clap peel” mechanism, force generation mechanisms evaluated. research indicates longitudinal performance mainly related parameters body, it can lead butterfly-inspired flapping air vehicles.

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Investigation of the Flow and Cavitation in a Butterfly Valve

Since knowledge on hydrodynamic torque of a butterfly valve is very important for butterfly valve design, its hydrodynamic torque is investigated in this paper. In reality, the investigation of the loss coefficient and torque from some experiments will take a long time and a lot of money. This paper presents a statistical study of the flow past the butterfly valve in a static analysis using com...

متن کامل

Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle

Inspired by superior flight performance of natural flight masters like birds and insects and based on the ventilating flaps that can be opened and closed by the changing air pressure around the wing, a new flapping wing type has been proposed. It is known that the net lift force generated by a solid wing in a flapping cycle is nearly zero. However, for the case of the ventilated wing, results f...

متن کامل

Resonance 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 کامل

An investigation into the longitudinal dynamics and control of a flapping wing micro air vehicle at hovering flight

This paper describes the research into the flight dynamics modelling and flight control of a flapping wing micro aerial vehicle (MAV). The equations of motion based on a multi-body representation of the vehicle and the flapping wings were derived and form the basis for the simulation program, which was developed using MATLAB and SIMULINK. The aerodynamic forces were obtained through experimenta...

متن کامل

Dipteran wing motor-inspired flapping flight versatility and effectiveness enhancement.

Insects are a prime source of inspiration towards the development of small-scale, engineered, flapping wing flight systems. To help interpret the possible energy transformation strategies observed in Diptera as inspiration for mechanical flapping flight systems, we revisit the perspective of the dipteran wing motor as a bistable click mechanism and take a new, and more flexible, outlook to the ...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Applied sciences

سال: 2021

ISSN: ['2076-3417']

DOI: https://doi.org/10.3390/app11062620