Effects of fluid-structure interaction on the aerodynamics of an insect wing

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In this paper, an insect wing structure is modeled based on data obtained from measurements on real hawkmoth (Manduca Sexta) wings. The aerodynamics of insect wings is simulated by an extended unsteady vortex-lattice method. The finite-element model of a flexible hawkmoth wing is built and validated. A computer program, which couples the finite-element model with the aerodynamic model, is used to study the effects of fluid-structure interaction. Some important features due to the fluid-structure interaction in hovering and forward flight are observed in the present study.
Publisher
SPIE
Issue Date
2016-03-22
Language
English
Citation

Bioinspiration, Biomimetics, and Bioreplication 2016

DOI
10.1117/12.2218781
URI
http://hdl.handle.net/10203/217219
Appears in Collection
AE-Conference Papers(학술회의논문)
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