ArticleBiomimetics (Basel, Switzerland)2023
Effect of Hindwings on the Aerodynamics and Passive Dynamic Stability of a Hovering Hawkmoth.
Article in Biomimetics (Basel, Switzerland), 2023. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 4 papers.
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Who cites it
4 citing papers in PubMed.
- Investigating the Mechanical Performance of Bionic Wings Based on the Flapping Kinematics of Beetle Hindwings.Biomimetics (Basel, Switzerland) · 2024Article
- Clap-and-Fling Mechanism of Climbing-Flight Coccinella Septempunctata.Biomimetics (Basel, Switzerland) · 2024Article
- Distributed State Estimation for Flapping-Wing Micro Air Vehicles with Information Fusion Correction.Biomimetics (Basel, Switzerland) · 2024Article
- A Novel Hybrid Deep Learning Method for Predicting the Flow Fields of Biomimetic Flapping Wings.Biomimetics (Basel, Switzerland) · 2024Article
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Authors and funding
3 authors.
Funding
Abstract
Insects are able to fly stably in the complex environment of the various gusts that occur in nature. In addition, many insects suffer wing damage in their lives, but many species of insects are capable of flying without their hindwings. Here, we evaluated the effect of hindwings on aerodynamics using a Navier-Stokes-based numerical model, and then the passive dynamic stability was evaluated by coupling the equation of motion in three degrees of freedom with the aerodynamic forces estimated by the CFD solver under large and small perturbation conditions. In terms of aerodynamic effects, the presence of the hindwings slightly reduces the efficiency for lift generation but enhances the partial LEV circulation and increases the downwash around the wing root. In terms of thrust, increasing the wing area around the hindwing region increases the thrust, and the relationship is almost proportional at the cycle-averaged value. The passive dynamic stability was not clearly affected by the presence of the hindwings, but the stability was slightly improved depending on the perturbation direction. These results may be useful for the integrated design of wing geometry and flight control systems in the development of flapping-winged micro air vehicles.
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