Please use this identifier to cite or link to this item:
Title: Two-wing clappers for micro-air vehicle
Authors: Liew, Wei Jian
Keywords: DRNTU::Engineering
Issue Date: 2016
Abstract: An experimental study was conducted to assess the aerodynamic benefits of using ‘Clap-and-Fling’ flapping flight mechanics for the development of Micro-Aerial Vehicle (MAV). The overall flight performance in terms of thrust generation of the ‘Clap-and-Fling’ flight was compared between the two different type of root chord with the wings which is “flexible root chord and fixed root chord” respectively. The experimental results clearly revealed that the ‘Clap-and-Fling’ mechanics with flexible root chord provided significant aerodynamic benefits. The thrust/frequency ratio and the thrust/power ratio are higher for the passive wings. Furthermore in term of power consumption, flexible root chord have less power consumption compare to the fixed wing. The thrust/power to frequency ratio also suggested that the flexible root chord is more efficient overall.
Rights: Nanyang Technological University
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)

Files in This Item:
File Description SizeFormat 
A147- Two Wing Clapper of MAV.pdf
  Restricted Access
2.19 MBAdobe PDFView/Open

Page view(s)

Updated on Apr 16, 2021


Updated on Apr 16, 2021

Google ScholarTM


Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.