This work aims to develop an integrated conceptual design process to assess the scalability and performance of propulsion systems of resonant motor-driven flapping wing vehicles. The developed process
In the fusion design process of the system, ill-conditioned features, that are not explicit in previous generation systems, may exhibit to negate the operation of the new-generation system. This type
This work aims to develop an integrated conceptual design process to assess the scalability and performance of propulsion systems of resonant motor-driven flapping wing vehicles. The developed process
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