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Project to optimise the design of a UAV with a range and payload requirement

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UAV-optimiser

Project to optimise the design of a UAV with a range and payload requirement

2D Analysis software iterates XFOIL to find the lowest drag aerofoil for a given aircraft mass

OpenVSP project aim: optimise wing parameters for maximum efficiency

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Project to optimise the design of a UAV with a range and payload requirement

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