Evidence map›Paper›PMID 42345713›Full record

ArticleBiomimetics (Basel, Switzerland)2026

Effects of Wing-Tail Coupling on Aerodynamic Performance of Flapping-Wing Aircraft.

Chao Wang, Longtian Zhang, Hao Liu, Kaicheng Yu, Jing Wu, Mingkang Zhu

Abstract read
In one paragraph

Article in Biomimetics (Basel, Switzerland), 2026. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Not yet cited in PubMed.

0numbers the graph read from it
0cells of the map it votes in
0citing papers in PubMed
–field-weighted citation impact
1 · What the graph read from it

What it found

Each row is one number read from the abstract, on the scale the paper reported it, with its interval. Left of the dashed line favours the treatment, right favours the comparator. Under each row is the sentence it came from. New to these charts? A ten-minute tutorial.

The abstract states no effect estimate the extractor could read, or names no intervention and outcome on the map, so this paper lights no cell and moves no belief. It is still indexed, cited and linked below.

2 · The registry

The trial behind it

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Neither the registry nor the abstract names a trial number. If this is a trial report, that itself is worth knowing.

3 · Its place in the literature

Who cites it

0 citing papers in PubMed.

No citing paper in PubMed yet.

4 · The record

Corrections and comments

PubMed lists nothing against this paper. Absence here is not a guarantee, only a check that was made.

5 · Who and what money

Authors and funding

6 authors.

Chao WangDepartment of Mechanical Engineering, Dongguan University of Technology, Dongguan 523808, China.ORCID 0000-0001-6645-4409
Longtian ZhangDepartment of Mechanical Engineering, Dongguan University of Technology, Dongguan 523808, China.
Hao LiuDepartment of Mechanical Engineering, Dongguan University of Technology, Dongguan 523808, China.
Kaicheng YuDepartment of Mechanical Engineering, Dongguan University of Technology, Dongguan 523808, China.
Jing WuDepartment of Mechanical Engineering, Dongguan University of Technology, Dongguan 523808, China.
Mingkang ZhuDepartment of Mechanical Engineering, Dongguan University of Technology, Dongguan 523808, China.

Funding

China Postdoctoral Science Foundation 2025M771401GuangDong Basic and Applied Basic Research Foundation 2024A1515140103National Natural Science Foundation of China 52005104
6 · The paper itself

Abstract

To address the limited understanding of the aerodynamic characteristics of bird-inspired flapping-wing aircraft across different flight phases and the unclear flow field interaction mechanisms between the wings and tail, this study performs three-dimensional numerical simulations based on a self-developed prototype using ANSYS Fluent and the overset mesh method. The aerodynamic effects of key tail parameters under different flight conditions are quantitatively evaluated, and the mechanisms of bidirectional wing-tail aerodynamic coupling are investigated. The results show that tail twist has a negligible influence on instantaneous lift and thrust during level flight, with a maximum variation of only 0.2 N, but significantly affects the overall aerodynamic moments of the aircraft. When the tail twist angle increases from 15° to 20°, the pitching moment increases by 6%. In contrast, during climbing flight, the tail pitch angle has a pronounced effect on lift and thrust, and its aerodynamic influence depends strongly on the aircraft angle of attack. At an aircraft angle of attack of 15°, the difference between the maximum and minimum cycle-averaged pitching moments reaches 0.2 N·m. Further analysis of vorticity fields and pressure distributions confirms the existence of distinct wing-tail aerodynamic coupling. The tail not only directly modifies the aerodynamic forces and moments acting on the aircraft but also alters the wing-generated flow structures, while the wing wake simultaneously influences the aerodynamic effectiveness of the tail. This bidirectional wing-tail aerodynamic coupling plays a critical role in shaping the aerodynamic response of the aircraft under different flight conditions. These findings clarify the aerodynamic roles of key tail parameters and reveal the underlying flow field interaction mechanisms across different flight phases, providing a theoretical basis for motion-parameter optimization and precise attitude control of bird-inspired flapping-wing aircraft.

Indexed as

aerodynamic characteristicsbird-inspired flapping-wing aircraftwing–tail aerodynamic coupling

Identifiers

PMID42345713
PMCPMC13296719

What Socratic holds

Textmetadata
LicenceCC BY
Read underepoch 390

Registered trials

None linked

Read under generation 80e0d062 · epoch 390. Bibliography from PubMed, PubMed Central and OpenAlex; grants from NIH RePORTER; trial links from ClinicalTrials.gov; estimates, votes and beliefs from the Socratic graph.