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Simulasi_Airfoil_NACA652415
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1 Geometry 1 Mesh 1 Simulation setup 0 ResultsAbout this project
Analisis Eksperimental Pengaruh Sudut Serang (Angle of Attack) terhadap Koefisien Lift dan Penentuan Titik Stall pada Airfoil NACA 65₂-415
