Evidence map›Paper›PMID 38611985›Full record

ArticleMaterials (Basel, Switzerland)2024

Non-Conventional Wing Structure Design with Lattice Infilled through Design for Additive Manufacturing.

Numan Khan, Valerio Acanfora, Aniello Riccio

Abstract read
In one paragraph

Article in Materials (Basel, Switzerland), 2024. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 4 papers.

0numbers the graph read from it
0cells of the map it votes in
4citing 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

4 citing papers in PubMed.

  1. Article
  2. Article
  3. Review
  4. Review
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

3 authors.

Numan KhanDepartment of Engineering, University of Campania "Luigi Vanvitelli", via Roma, 29, 81031 Aversa, Italy.ORCID 0000-0002-8649-224X
Valerio AcanforaDepartment of Engineering, University of Campania "Luigi Vanvitelli", via Roma, 29, 81031 Aversa, Italy.ORCID 0000-0002-1222-5683
Aniello RiccioDepartment of Engineering, University of Campania "Luigi Vanvitelli", via Roma, 29, 81031 Aversa, Italy.ORCID 0000-0001-7426-6803

Funding

No grant is acknowledged in the PubMed record.

6 · The paper itself

Abstract

Lightweight structures with a high stiffness-to-weight ratio always play a significant role in weight reduction in the aerospace sector. The exploration of non-conventional structures for aerospace applications has been a point of interest over the past few decades. The adaptation of lattice structure and additive manufacturing in the design can lead to improvement in mechanical properties and significant weight reduction. The practicality of the non-conventional wing structure with lattices infilled as a replacement for the conventional spar-ribs wing is determined through finite element analysis. The optimal lattice-infilled wing structures are obtained via an automated iterative method using the commercial implicit modeling tool nTop and an ANSYS workbench. Among five different types of optimized lattice-infilled structures, the Kelvin lattice structure is considered the best choice for current applications, with comparatively minimal wing-tip deflection, weight, and stress. Furthermore, the stress distribution dependency on the lattice-unit cell type and arrangement is also established. Conclusively, the lattice-infilled structures have shown an alternative innovative design approach for lightweight wing structures.

Indexed as

additive manufacturingfinite element analysislattice-infilled designlightweight structuresnon-conventional wing structure

Identifiers

PMID38611985
PMCPMC11012710

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Registered trials

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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.