Testing and evaluation of flapping wing mechanism
Date of Issue2009
School of Mechanical and Aerospace Engineering
Facility for Analysis, Characterisation, Testing and Simulation
Defence Science Organisation (DSO)
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.
Final Year Project (FYP)
Nanyang Technological University