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Design of a small-scale aircraft model is considered as one of the most essential methods for verifying new concepts. We developed scaling methods for a novel aircraft configuration with hinge wingtips.
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This page is a summary of: Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge, AIAA Journal, April 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063646.
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