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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主要作者: Lim, Qing Long
其他作者: School of Mechanical and Aerospace Engineering
格式: Final Year Project
語言:English
出版: 2014
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在線閱讀:http://hdl.handle.net/10356/61329
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機構: Nanyang Technological University
語言: English

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