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Numerical Analysis of NACA 4415 Airfoil Performance

التحليل العددي لأداء مقطع جناح NACA 4415

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 Publication date 2016
and research's language is العربية
 Created by Shamra Editor




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The aerodynamic performance of an airfoil of the shape NACA 4415 was investigated using CFD numerical analysis.

References used
ANDERSON J., 2001 - Fundamentals of Aerodynamics McGraw Hill, 3rd edition, USA, 892p
HOFFMANN K., CHIANG S., 2000 - Computational Fluid Dynamics Engineering Education System, 4th edition (3 volumes), USA, 175p
ABBOT I. VON DOENHOFF A., 1959 - Theory of Wing Sections, Including a Summary of Airfoil Data Dover Inc., USA, 693p
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يتحدث المحتوى عن طرق الاستيفاء بالتحليل العددي بشكل برمجي وهما طريقتين طريقة استيفاء لاغرانج وطريقة سبلاين الخطية بلغة c++ والجافا وهما موجودين على شكل تطبيق اندرويد
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