ArticleNature communications2023
Digital mapping of surface turbulence status and aerodynamic stall on wings of a flying aircraft.
Article in Nature communications, 2023. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 10 papers.
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.
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Who cites it
10 citing papers in PubMed.
- A triboelectric airflow field sensor enables cross-scale multi-parameter sensing in meter-scale flapping-wing aircrafts.Science advances · 2026Article
- Flexible, super-resolution skin with in-sensor hyperdimensional computing for real-time pressure field perception.Science advances · 2026Article
- Triboelectric Nanogenerators in Military: Recent Progress and Critical Challenges.Nano-micro letters · 2026Review
- Triboelectric Nanogenerators for Future Space Missions.Nano-micro letters · 2026Review
- Bifurcation and synchronization analysis in a stall-flutter aeroelastic system under varying preset angles and frequency ratios.Scientific reports · 2025Article
- Bioinspired twist-hyperbolic metamaterial for impact buffering and self-powered real-time sensing in UAVs.Science advances · 2025Article
- Self-Powered, Flexible, Transparent Tactile Sensor Integrating Sliding and Proximity Sensing.Materials (Basel, Switzerland) · 2025Article
- Avian-inspired embodied perception in biohybrid flapping-wing robotics.Nature communications · 2024Article
- Creep-free polyelectrolyte elastomer for drift-free iontronic sensing.Nature materials · 2024Article
- Towards extending the aircraft flight envelope by mitigating transonic airfoil buffet.Nature communications · 2024Article
Corrections and comments
PubMed lists nothing against this paper. Absence here is not a guarantee, only a check that was made.
Authors and funding
9 authors.
Funding
No grant is acknowledged in the PubMed record.
Abstract
Real-time monitoring of flow turbulence is very difficult but extremely important in fluid dynamics, which plays an important role in flight safety and control. Turbulence can cause airflow to detach at the end of the wings, potentially resulting in the aerodynamic stall of aircraft and causing flight accidents. Here, we developed a lightweight and conformable system on the wing surface of aircraft for stall sensing. Quantitative data about airflow turbulence and the degree of boundary layer separation are provided in situ using conjunct signals provided by both triboelectric and piezoelectric effects. Thus, the system can visualize and directly measure the airflow detaching process on the airfoil, and senses the degree of airflow separation during and after a stall for large aircraft and unmanned aerial vehicles.
Identifiers
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Registered trials
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.