Micro air vehicles : flapping wing propulsion

• المؤلف الرئيسي: Koay, Say Seng.
• مؤلفون آخرون: Jorg Uwe Schluter
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2011
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aircraft
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/45669

This Final Year Report (FYP) investigated the aerodynamic effects of a flapping wing. A water tunnel facility was used in the experiments, testing the effects of a wing in heaving motion on a constant, steady flow. The wing used was a straight wing of airfoil NACA 0012. Two different methods were us...