Evidence map›Paper›PMID 34234957›Full record

ArticleRoyal Society open science2021

Effects of uniform vertical inflow perturbations on the performance of flapping wings.

Soudeh Mazharmanesh, Jace Stallard, Albert Medina, Alex Fisher, Noriyasu Ando, Fang-Bao Tian, John Young, Sridhar Ravi

Open access · goldAbstract read
In one paragraph

Article in Royal Society open science, 2021. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 1 paper.

0numbers the graph read from it
0cells of the map it votes in
1citing papers in PubMed
6.2field-weighted citation impact, top 4% 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

1 citing paper in PubMed, 6 citations in OpenAlex.

  1. Article
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

8 authors at 4 institutions in 3 countries.

Soudeh MazharmaneshSchool of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.ORCID 0000-0002-3263-760X
Jace StallardSchool of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.
Albert MedinaUS Air Force Research Laboratory, Wright-Patterson Air Force Base, OH 45433, USA.
Alex FisherSchool of Engineering, RMIT University, Melbourne, 3083, Australia.
Noriyasu AndoDepartment of System Life Engineering, Maebashi Institute of Technology, Maebashi 371-0816, Japan.
Fang-Bao TianSchool of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.
John YoungSchool of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.ORCID 0000-0002-8671-990X
Sridhar RaviSchool of Engineering and Information Technology, University of New South Wales, Canberra, ACT 2600, Australia.ORCID 0000-0001-7397-9713
University of Canberra · AUMaebashi Institute of Technology · JPRMIT University · AUWright-Patterson Air Force Base · US

Funding

No grant is acknowledged in the PubMed record.

6 · The paper itself

Abstract

Flapping wings have attracted significant interest for use in miniature unmanned flying vehicles. Although numerous studies have investigated the performance of flapping wings under quiescent conditions, effects of freestream disturbances on their performance remain under-explored. In this study, we experimentally investigated the effects of uniform vertical inflows on flapping wings using a Reynolds-scaled apparatus operating in water at Reynolds number ≈ 3600. The overall lift and drag produced by a flapping wing were measured by varying the magnitude of inflow perturbation from

Indexed as

disturbancesflapping wingsvertical inflowswake interactionwind gusts

Identifiers

PMID34234957
PMCPMC8242829
OpenAlexW3175601789

What OpenQuestion 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 OpenQuestion graph.