Dynamic Behavior of Ti/Ti Single-Lap Laminated Structure with a Large-Diameter Bolt-Based Electromagnetic Force: Numerical Simulation and Experimental Verification.

Duquan Zuo, Shaoqing Jin, Tianyu Xu, Minghao Zhang, Mengyang Cui, Haolin Ding, Yaoming Fu

Abstract read

In one paragraph

Article in Materials (Basel, Switzerland), 2025. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Not yet cited in PubMed.

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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

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0 citing papers in PubMed.

No citing paper in PubMed yet.

4 · The record

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5 · Who and what money

Authors and funding

7 authors.

Duquan ZuoSichuan Province Engineering Technology Research Center of General Aircraft Maintenance, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.ORCID 0000-0002-5053-0400

Shaoqing JinCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.

Tianyu XuCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.

Minghao ZhangSchool of Materials Science and Engineering, Northwestern Polytechnical University, 127 West Youyi Road, Xi'an 710072, China.

Mengyang CuiCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.

Haolin DingCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.

Yaoming FuSichuan Province Engineering Technology Research Center of General Aircraft Maintenance, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.

Funding

Fundamental Research Funds for the Central Universities NO. 24CAFUC07002, NO. J2023-032National Natural Science Foundation of China NO. 52275165Sichuan Province Engineering Technology Research Center of General Aircraft Maintenance NO. GAMRC2023ZD03Sichuan Science and Technology Program NO. 2023YFG0165, NO.2023NSFSC0372

6 · The paper itself

Abstract

Electromagnetic force installation is recognized as a viable solution for interference-fit issues in large-diameter bolts. However, the dynamic mechanical behavior of the joint during installation has not been fully clarified. This study investigated the dynamic mechanical behavior of large-diameter Ti/Ti interference-fit bolted joints during electromagnetic installation through numerical simulation and experimental validation. The simulation results indicate uniform deformation at the inlet of the bore wall under interference levels, with a maximum displacement variance of 21.1 μm

Indexed as

dynamic mechanical behaviorelectromagnetic forcefinite element analysisinterference-fit bolted jointlarge-diameter boltTC4 alloy

Identifiers

PMID40271648

DOI10.3390/ma18071473

PMCPMC11989611

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LicenceCC BY

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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.