Evidence map›Paper›PMID 25079868›Full record

ArticleJournal of the Royal Society, Interface2014

Hummingbird wing efficacy depends on aspect ratio and compares with helicopter rotors.

Jan W Kruyt, Elsa M Quicazán-Rubio, GertJan F van Heijst, Douglas L Altshuler, David Lentink

Open access · bronzeAbstract readComparative Study
In one paragraph

Article in Journal of the Royal Society, Interface, 2014. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 30 papers.

0numbers the graph read from it
0cells of the map it votes in
30citing papers in PubMed
199.5field-weighted citation impact, top 1% of its field
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

Trials whose registry record cites this paper, or whose number appears in the abstract. A trial that started after this paper was published is citing it as background, not reporting it.

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

30 citing papers in PubMed, 113 citations in OpenAlex.

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  4. The spatiotemporal richness of hummingbird wing deformations.The Journal of experimental biology · 2024
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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

5 authors at 4 institutions in 3 countries.

Jan W KruytMechanical Engineering, Stanford University, 416 Escondido Mall, Stanford, CA 94305, USA Experimental Zoology Group, Wageningen University, PO Box 338, 6700 AH Wageningen, The Netherlands.
Elsa M Quicazán-RubioExperimental Zoology Group, Wageningen University, PO Box 338, 6700 AH Wageningen, The Netherlands.
GertJan F van HeijstPhysics Department, Eindhoven University of Technology, PO Box 516, 5600 MB Eindhoven, The Netherlands.
Douglas L AltshulerDepartment of Zoology, University of British Columbia, 4200-6270 University Boulevard, Vancouver, British Columbia, Canada V6T1Z4.
David LentinkMechanical Engineering, Stanford University, 416 Escondido Mall, Stanford, CA 94305, USA dlentink@stanford.edu.
Stanford University · USEindhoven University of Technology · NLUniversity of British Columbia · CAWageningen University & Research · NL

Funding

No grant is acknowledged in the PubMed record.

6 · The paper itself

Abstract

Hummingbirds are the only birds that can sustain hovering. This unique flight behaviour comes, however, at high energetic cost. Based on helicopter and aeroplane design theory, we expect that hummingbird wing aspect ratio (AR), which ranges from about 3.0 to 4.5, determines aerodynamic efficacy. Previous quasi-steady experiments with a wing spinner set-up provide no support for this prediction. To test this more carefully, we compare the quasi-steady hover performance of 26 wings, from 12 hummingbird taxa. We spun the wings at angular velocities and angles of attack that are representative for every species and measured lift and torque more precisely. The power (aerodynamic torque × angular velocity) required to lift weight depends on aerodynamic efficacy, which is measured by the power factor. Our comparative analysis shows that AR has a modest influence on lift and drag forces, as reported earlier, but interspecific differences in power factor are large. During the downstroke, the power required to hover decreases for larger AR wings at the angles of attack at which hummingbirds flap their wings (p < 0.05). Quantitative flow visualization demonstrates that variation in hover power among hummingbird wings is driven by similar stable leading edge vortices that delay stall during the down- and upstroke. A side-by-side aerodynamic performance comparison of hummingbird wings and an advanced micro helicopter rotor shows that they are remarkably similar.

Indexed as

AircraftAnimalsBiomechanical PhenomenaBirdsFlight, AnimalWings, Animalaspect ratiohoveringhummingbirdperformancequasi-steadywing

Identifiers

PMID25079868
PMCPMC4233735
OpenAlexW2148493613

What OpenQuestion holds

Textmetadata
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 OpenQuestion graph.