Evidence map›Paper›PMID 39770177›Full record

ArticleMicromachines2024

Screen-Printed PVDF Piezoelectric Pressure Transducer for Unsteadiness Study of Oblique Shock Wave Boundary Layer Interaction.

Bei Wang, Cosimo Corsi, Thomas Weiland, Zhenyu Wang, Thomas Grund, Olaf Pohl, Johannes Max Bienia, Julien Weiss, Ha Duong Ngo

Abstract read
PubMed Full text at PMC Publisher
In one paragraph

Article in Micromachines, 2024. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 3 papers.

0numbers the graph read from it
0cells of the map it votes in
3citing 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

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

3 citing papers in PubMed.

  1. Article
  2. Article
  3. 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

9 authors.

Bei WangDepartment of Microsystem Technology, University of Applied Sciences Berlin, 12459 Berlin, Germany.ORCID 0000-0003-4329-7396
Cosimo CorsiDepartment of Aerodynamics Engineer, Technical University of Berlin, 10587 Berlin, Germany.
Thomas WeilandDepartment of Microsystem Technology, University of Applied Sciences Berlin, 12459 Berlin, Germany.
Zhenyu WangDeye Neue Enerige Gmbh, Nordostpark 98-102, 90411 Nürnberg, Germany.
Thomas GrundDepartment of Aerodynamics Engineer, Technical University of Berlin, 10587 Berlin, Germany.
Olaf PohlDepartment of Microsystem Technology, University of Applied Sciences Berlin, 12459 Berlin, Germany.
Johannes Max BieniaDepartment of Microsystem Technology, University of Applied Sciences Berlin, 12459 Berlin, Germany.
Julien WeissDepartment of Aerodynamics Engineer, Technical University of Berlin, 10587 Berlin, Germany.
Ha Duong NgoDepartment of Microsystem Technology, University of Applied Sciences Berlin, 12459 Berlin, Germany.ORCID 0000-0002-0294-537X

Funding

Bundesministerium für Wirtschaft und Klimaschutz This research was funded by BMWK (Bundesministerium für Wirtschaft und Klimaschutz) research and innovation program UmTrieb.
6 · The paper itself

Abstract

Shock wave boundary/layer interactions (SWBLIs) are critical in high-speed aerodynamic flows, particularly within supersonic regimes, where unsteady dynamics can induce structural fatigue and degrade vehicle performance. Conventional measurement techniques, such as pressure-sensitive paint (PSP), face limitations in frequency response, calibration complexity, and intrusive instrumentation. Similarly, MEMS-based sensors, like Kulite

Indexed as

crosstalk effectdynamic response in frequency domainFEM simulationpiezoelectric pressure transducePVDFshock wave/boundary layer interaction (SWBLI)supersonicunsteadinesswall pressure

Identifiers

PMID39770177
PMCPMC11676075

What OpenQuestion holds

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LicenceCC BY
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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.