Vortex evolution near the Coanda surface of a circulation control airfoil with pulsed actuation

A special vortex evolution process was found near the Coanda surface for circulation control airfoil with pulsed actuation. For the jet-on process, two successive shedding vortices from the lower lip edge and the separation vortex on the Coanda surface collide and interact with each other, and perio...

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Main Authors: Quanbing Sun, Zhiwei Shi, Weilin Zhang, Sinuo Chen, Jie Chen
Format: Article
Language:English
Published: AIP Publishing LLC 2022-12-01
Series:AIP Advances
Online Access:http://dx.doi.org/10.1063/5.0123797
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author Quanbing Sun
Zhiwei Shi
Weilin Zhang
Sinuo Chen
Jie Chen
author_facet Quanbing Sun
Zhiwei Shi
Weilin Zhang
Sinuo Chen
Jie Chen
author_sort Quanbing Sun
collection DOAJ
description A special vortex evolution process was found near the Coanda surface for circulation control airfoil with pulsed actuation. For the jet-on process, two successive shedding vortices from the lower lip edge and the separation vortex on the Coanda surface collide and interact with each other, and periodic vortex shedding forms after several vortex shedding and collision cycles. For the jet-off process, the periodic shedding vortices were replaced by a row of vortices with reverse rotation direction from the upper lip edge, and then reverse vortices broke into small-scale vortices.
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spelling doaj.art-6b28d93ffb8147bab926a338b02db9882023-01-19T16:47:09ZengAIP Publishing LLCAIP Advances2158-32262022-12-011212125001125001-610.1063/5.0123797Vortex evolution near the Coanda surface of a circulation control airfoil with pulsed actuationQuanbing Sun0Zhiwei Shi1Weilin Zhang2Sinuo Chen3Jie Chen4College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, ChinaCollege of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, ChinaCollege of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, ChinaCollege of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, ChinaCollege of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, ChinaA special vortex evolution process was found near the Coanda surface for circulation control airfoil with pulsed actuation. For the jet-on process, two successive shedding vortices from the lower lip edge and the separation vortex on the Coanda surface collide and interact with each other, and periodic vortex shedding forms after several vortex shedding and collision cycles. For the jet-off process, the periodic shedding vortices were replaced by a row of vortices with reverse rotation direction from the upper lip edge, and then reverse vortices broke into small-scale vortices.http://dx.doi.org/10.1063/5.0123797
spellingShingle Quanbing Sun
Zhiwei Shi
Weilin Zhang
Sinuo Chen
Jie Chen
Vortex evolution near the Coanda surface of a circulation control airfoil with pulsed actuation
AIP Advances
title Vortex evolution near the Coanda surface of a circulation control airfoil with pulsed actuation
title_full Vortex evolution near the Coanda surface of a circulation control airfoil with pulsed actuation
title_fullStr Vortex evolution near the Coanda surface of a circulation control airfoil with pulsed actuation
title_full_unstemmed Vortex evolution near the Coanda surface of a circulation control airfoil with pulsed actuation
title_short Vortex evolution near the Coanda surface of a circulation control airfoil with pulsed actuation
title_sort vortex evolution near the coanda surface of a circulation control airfoil with pulsed actuation
url http://dx.doi.org/10.1063/5.0123797
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