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Performance of passively pitching flapping wings in the presence of vertical inflows.
Mazharmanesh, Soudeh; Stallard, Jace; Medina, Albert; Fisher, Alex; Ando, Noriyasu; Tian, Fang-Bao; Young, John; Ravi, Sridhar.
Afiliación
  • Mazharmanesh S; School of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.
  • Stallard J; School of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.
  • Medina A; U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, OH 45433, United States of America.
  • Fisher A; School of Engineering, RMIT University, Melbourne, 3083, Australia.
  • Ando N; Department of System Life Engineering, Maebashi Institute of Technology, Maebashi, 371-0816, Japan.
  • Tian FB; School of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.
  • Young J; School of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.
  • Ravi S; School of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.
Bioinspir Biomim ; 16(5)2021 07 15.
Article en En | MEDLINE | ID: mdl-34139680
ABSTRACT
The successful implementation of passively pitching flapping wings strongly depends on their ability to operate efficiently in wind disturbances. In this study, we experimentally investigated the interaction between a uniform vertical inflow perturbation and a passive-pitching flapping wing using a Reynolds-scaled apparatus operating in water at Reynolds number ≈3600. A parametric study was performed by systematically varying the Cauchy number (Ch) of the wings from 0.09 to 11.52. The overall lift and drag, and pitch angle of the wing were measured by varying the magnitude of perturbation fromJVert= -0.6 (downward inflow) toJVert= 0.6 (upward inflow) at eachCh, whereJVertis the ratio of the inflow velocity to the wing's velocity. We found that the lift and drag had remarkably different characteristics in response to bothChandJVert. Across allCh, while mean lift tended to increase as the inflow perturbation varied from -0.6 to 0.6, drag was significantly less sensitive to the perturbation. However effect of the vertical inflow on drag was dependent onCh, where it tended to vary from an increasing to a decreasing trend asChwas changed from 0.09 to 11.52. The differences in the lift and drag with perturbation magnitude could be attributed to the reorientation of the net force over the wing as a result of the interaction with the perturbation. These results highlight the complex interactions between passively pitching flapping wings and freestream perturbations and will guide the design of miniature flying crafts with such architectures.
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Texto completo: 1 Colección: 01-internacional Base de datos: MEDLINE Asunto principal: Vuelo Animal / Modelos Biológicos Tipo de estudio: Prognostic_studies Límite: Animals Idioma: En Revista: Bioinspir Biomim Asunto de la revista: BIOLOGIA / ENGENHARIA BIOMEDICA Año: 2021 Tipo del documento: Article País de afiliación: Australia

Texto completo: 1 Colección: 01-internacional Base de datos: MEDLINE Asunto principal: Vuelo Animal / Modelos Biológicos Tipo de estudio: Prognostic_studies Límite: Animals Idioma: En Revista: Bioinspir Biomim Asunto de la revista: BIOLOGIA / ENGENHARIA BIOMEDICA Año: 2021 Tipo del documento: Article País de afiliación: Australia