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Hasil Unplag_Effect of Angle of Attack on Airfoil NACA 0012 Performance

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Submission date: 20-Jan-2022 06:14AM (UTC+0700) Submission ID: 1744414532

File name: Effect_of_Angle_of_Attack_on_Airfoil_NACA_0012_Performance.pdf (279.36K) Word count: 3742

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Effect_of_Angle_of_Attack_on_Airfoil_NACA_0012_Performan…

ORIGINALITY REPORT

PRIMARY SOURCES

www.mdpi.com

Internet Source

"Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications", American Institute of Aeronautics and Astronautics (AIAA), 2001

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www.semanticscholar.org

Internet Source

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