ArticleScientific reports2025
Flexural performance of shape memory alloy/CF-PEKK fiber metal laminates for aircraft morphing under varied temperature conditions.
Article in Scientific reports, 2025. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 1 paper.
What it found
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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.
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.
Who cites it
1 citing paper in PubMed.
- Bending Behavior of Fiber Metal Laminate Plates Under Thermo-Mechanical Loads.Materials (Basel, Switzerland) · 2025Article
Corrections and comments
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Authors and funding
3 authors.
Funding
Abstract
In this study, novel Fiber Metal Laminates (FMLs) were manufactured using Nickel Titanium (NiTi) sheets together with Carbon Fiber-Polyetherketoneketone (CF-PEKK) prepregs for different aerospace applications. We have investigated the effect of various temperatures on the flexural properties of NiTi/CF-PEKK FMLs. Prior to manufacture, NiTi sheets were anodized to improve the adhesion between the metal surface with the prepreg. The laminate was then compression molded in a hot-press. The flexural response of manufactured FMLs was investigated at various temperature conditions encompassing martensite and austenite phase of NiTi and glass transition temperature (T
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