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Prediction of aerodynamic loads and stability derivatives using the unsteady Source and Doublet Panel Method for preliminary aircraft design

Dimitriadis, Grigorios; Panagiotou, Periklis; Dimopoulos, Thomas et al.

2024 • AIAA SciTech 2024 Forum and Exhibition

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129 AIAA 2024-0239.pdf

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129 AIAA 2024-0239.pdf

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