2026-10-09T19:27:07Z
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2026-10-01T10:32:22Z
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category_33020
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Supplementary Figure 1
Kyung Jun Paul Lee (22632364)
Diaa Zekry (22632367)
Ahmed K Othman (22632370)
Aimy Wissa (22632373)
Marianne Alleyne (4318228)
Biomolecular modelling and design
Biomaterials
Biomimetics
Biomechanics
<table><tr><td><p dir="ltr"><br>Chord-wise corrugated-sections from the micro-CT scans of the hindwing and estimated camber lines using moving average smoothing. The percentages denote the semi-span location, with low values representing the cross-section near the root (proximal) and high values representing the cross-section near the tip (distal) of the wing. <i>f</i> is the maximum camber magnitude, <i>x</i><sub><em>f</em></sub> is the chord-wise location of the maximum camber, and <i>c</i> is the chord length at the given semi-span location. The chord-wise location of the maximum camber is denoted as a red dot. The point of inflection of the camber line at 50%, 60%, 70% semi-span location is shown in a blue cross.</p></td></tr></table><p></p>
2025-11-17T13:08:45Z
Image
Figure
10.6084/m9.figshare.30639040.v4
https://figshare.com/articles/figure/Supplementary_Video_1_from_From_Grasshoppers_to_Gliders_Evaluating_the_Role_of_Hindwing_Morphology_in_Gliding_Flight/30639040
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