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Effect of slenderness on optimal shapes.
Effect of slenderness on optimal shapes. δ*-Optimal structures (from Table 1) with twofold reflection symmetry (top) and skew symmetry (bottom). Propellers’ aspect ratio varies from left to right from 1:3 to 1:7 (top) and from 1:4 to 1:8 (bottom). The (red) arrow in the bottom panel corresponds to the direction of the magnetic moment m maximizing δ*. Yoni Mirzae et al. Sci. Robotics 2018;3:eaas8713 Copyright © 2018 The Authors, some rights reserved; exclusive licensee American Association for the Advancement of Science. No claim to original U.S. Government Works
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