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Cited article:

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Aircraft Engineering and Aerospace Technology 94 (6) 965 (2022)
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Accuracy of the Gamma Re-Theta Transition Model for Simulating the DU-91-W2-250 Airfoil at High Reynolds Numbers

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Computational analysis of NACA 0010 at moderate to high Reynolds number using 2D panel method

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MOJ Applied Bionics and Biomechanics 4 (5) 125 (2020)
https://doi.org/10.15406/mojabb.2020.04.00147