Flapping membrane wing: a prediction towards inter-domain flight

The purpose of this research is to gain initial knowledge and to predict the sustainability of an all-weather Micro-Aerial-Vehicle (MAV). The observed parameters are: the maximum coefficient of lift, CL and the changes in CL after impact, the fluctuation of CL upon entering simulated rain environmen...

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Bibliographic Details
Main Authors: Abas, M. F., Aftab, Syed Mohammed Aminuddin, Mohd Rafie, Azmin Shakrine, Yusoff, Hamid, Ahmad, Kamarul Arifin
Format: Article
Language:English
Published: Universiti Putra Malaysia Press 2016
Online Access:http://psasir.upm.edu.my/id/eprint/29374/1/17%20JST%28S%29-0024-2016.pdf
http://psasir.upm.edu.my/id/eprint/29374/
http://www.pertanika.upm.edu.my/Pertanika%20PAPERS/JST%20Vol.%2024%20(2)%20Jul.%202016/17%20JST(S)-0024-2016.pdf
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Institution: Universiti Putra Malaysia
Language: English