تم في هذا البحث دراسة الأداء الأيروديناميكي لمقطع جناح NACA 4415, اعتمادا على التحليل العددي باستخدام تقنيات ميكانيك الموائع الحسابي CFD.
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
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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