Micro air vehicles : flapping wing propulsion

• 主要作者: Koay, Say Seng.
• 其他作者: Jorg Uwe Schluter
• 格式: Final Year Project
• 語言: English
• 出版: 2011
• 主題: DRNTU::Engineering::Aeronautical engineering::Aircraft
• 在線閱讀: 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...