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A. Benaissa

Royal Military College of Canada

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Pitch–Heave Symmetric Stall Flutter of a NACA0012 at Transitional Reynolds Numbers

2020 AIAA Journal
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Mode and regime identification for a static NACA0012 airfoil at transitional Reynolds numbers

2020 Mechanics & Industry
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Aerodynamic-Aeroacoustic Investigation of Rotating Stall in Conventional and Skewed Rotors

2004
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