Aerodynamic response of micro rotary wings in wind perturbation

One high fidelity numerical method is extended to compute the unsteady aerodynamic loads when micro rotary wings suffer wind. The unsteady solutions are obtained by solving Navier-Stokes equations, where field velocity method is proposed to carry out the atmospheric perturbation. The convective term...

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Main Authors: Li Xu, Shuo Wu, Yuan Chai
Format: Article
Language:English
Published: JVE International 2018-08-01
Series:Journal of Vibroengineering
Subjects:
Online Access:https://www.jvejournals.com/article/18911
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spelling doaj-7c15cf06d19b45e4969b9cddc76a4ba22020-11-24T21:19:07ZengJVE InternationalJournal of Vibroengineering1392-87162538-84602018-08-012052175218710.21595/jve.2018.1891118911Aerodynamic response of micro rotary wings in wind perturbationLi Xu0Shuo Wu1Yuan Chai2School of Mathematics and Physics, Shanghai University of Electric Power, Shanghai, ChinaSchool of Mathematics and Physics, Shanghai University of Electric Power, Shanghai, ChinaSchool of Mathematics and Physics, Shanghai University of Electric Power, Shanghai, ChinaOne high fidelity numerical method is extended to compute the unsteady aerodynamic loads when micro rotary wings suffer wind. The unsteady solutions are obtained by solving Navier-Stokes equations, where field velocity method is proposed to carry out the atmospheric perturbation. The convective terms are approximated by a high order WENO-Roe scheme, and time advance is performed by an implicit scheme of dual time stepping which can guarantee a degree of efficiency. Moving overset grids are used to facilitate the implement of rotational motion of rotary wings and relative movements between rotary wings, as well as the atmospheric perturbation. The results reveal that small atmospheric perturbation has an important impact on the flows of micro rotary wings under low Reynolds number. The response of thrust coefficient presents periodic fluctuation and its amplitude is proportional to that of wind disturbance, which provides the clue for active control research of rotary wing aircraft.https://www.jvejournals.com/article/18911atmospheric perturbationaerodynamic responseviscous flows around micro rotary wingsmoving overset gridsfield velocity method
collection DOAJ
language English
format Article
sources DOAJ
author Li Xu
Shuo Wu
Yuan Chai
spellingShingle Li Xu
Shuo Wu
Yuan Chai
Aerodynamic response of micro rotary wings in wind perturbation
Journal of Vibroengineering
atmospheric perturbation
aerodynamic response
viscous flows around micro rotary wings
moving overset grids
field velocity method
author_facet Li Xu
Shuo Wu
Yuan Chai
author_sort Li Xu
title Aerodynamic response of micro rotary wings in wind perturbation
title_short Aerodynamic response of micro rotary wings in wind perturbation
title_full Aerodynamic response of micro rotary wings in wind perturbation
title_fullStr Aerodynamic response of micro rotary wings in wind perturbation
title_full_unstemmed Aerodynamic response of micro rotary wings in wind perturbation
title_sort aerodynamic response of micro rotary wings in wind perturbation
publisher JVE International
series Journal of Vibroengineering
issn 1392-8716
2538-8460
publishDate 2018-08-01
description One high fidelity numerical method is extended to compute the unsteady aerodynamic loads when micro rotary wings suffer wind. The unsteady solutions are obtained by solving Navier-Stokes equations, where field velocity method is proposed to carry out the atmospheric perturbation. The convective terms are approximated by a high order WENO-Roe scheme, and time advance is performed by an implicit scheme of dual time stepping which can guarantee a degree of efficiency. Moving overset grids are used to facilitate the implement of rotational motion of rotary wings and relative movements between rotary wings, as well as the atmospheric perturbation. The results reveal that small atmospheric perturbation has an important impact on the flows of micro rotary wings under low Reynolds number. The response of thrust coefficient presents periodic fluctuation and its amplitude is proportional to that of wind disturbance, which provides the clue for active control research of rotary wing aircraft.
topic atmospheric perturbation
aerodynamic response
viscous flows around micro rotary wings
moving overset grids
field velocity method
url https://www.jvejournals.com/article/18911
work_keys_str_mv AT lixu aerodynamicresponseofmicrorotarywingsinwindperturbation
AT shuowu aerodynamicresponseofmicrorotarywingsinwindperturbation
AT yuanchai aerodynamicresponseofmicrorotarywingsinwindperturbation
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