Experimental and numerical data from comparative analysis of candidate structural models for active camber morphing

Ke Huang1, Jiaying Zhang1

  • 1School of Aeronautic Science and Engineering, Beihang University, Beijing 100190, China.

Data in Brief
|July 13, 2026
PubMed
Summary

This study provides modal test data for FDM-printed PLA and aluminum cantilever plates. The dataset serves as a benchmark for validating structural models of morphing wings.

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