STUDI AKURASI SOLUSI NUMERIK DAN ANALISIS AERODINAMIKA AIRFOIL NACA SIMETRIK PADA BILANGAN REYNOLDS RENDAH

• المؤلف الرئيسي: Ayusyalita, Raras
• التنسيق: Final Project
• اللغة: Indonesia
• الوصول للمادة أونلاين: https://digilib.itb.ac.id/gdl/view/33811

The performance of airfoils at low Reynolds number has been a research interest in the field of fluid dynamics in recent decades. This attracts higher interest in the development of Unmanned Air Vehicle (UAV) including Micro Air Vehicle (MAV) and the development of utilization of renewable energy, s...