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At early stages of the aircraft design process, the stability of the future aircraft is usually predicted using empirical methods. We develop and validate a novel method for stability calculations based on a potential flow model
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This page is a summary of: Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method, Journal of Aircraft, July 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037747.
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