Testing and evaluation of flapping wing mechanism

• Main Author: Indra Gunawan
• Other Authors: Low Kin Huat
• Format: Final Year Project
• Language: English
• Published: 2009
• Subjects: DRNTU::Engineering::Aeronautical engineering::Aircraft
• Online Access: http://hdl.handle.net/10356/16105
• Institution: Nanyang Technological University

Design of the different wing designs which is fixed onto the flapping mechanism known as Ornithopter. Apparatus such as whirling arm test rig and the wind tunnel are used to test and evaluate the flight performance and characteristic of the different wing designs used onto the flapping mechanism.