Mass and aerodynamic properties characterization of a non-linearly damped flapping mechanism

This work aims at the experimental estimations of wing's aerodynamic and mass properties of a motor-driven flapper which is subjected to nonlinear aerodynamic damping in its operation. Analytical model is built to express the dynamics of the flapping mechanism and static experiments are carried...

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Bibliographic Details
Main Author: Lim, Qing Long
Other Authors: School of Mechanical and Aerospace Engineering
Format: Final Year Project
Language:English
Published: 2014
Subjects:
Online Access:http://hdl.handle.net/10356/61329
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Institution: Nanyang Technological University
Language: English