DocumentCode :
3596379
Title :
Acoustic comparison of PET and Latex wings for flapping micro-air-vehicles
Author :
Lung-Jieh Yang ; Marimuthu, Suseendar
Author_Institution :
Mech. & Electromech. Eng., Tamkang Univ., Taipei, Taiwan
fYear :
2015
Firstpage :
172
Lastpage :
174
Abstract :
This paper presents the hyper-elastic Latex film as the new material for flapping wings novelly. Compared to one of the conventional flapping wings using PET, the new Latex wing reduces the noise with 15.93 dB at least. Both wings have a wingspan of 20 cm and work at the flapping frequency of 13.3 Hz. The leading edge spars and the stiffened ribs of both wings are made of carbon fiber. This newly developed Latex wing is believed to be useful to the application of stealth micro-air-vehicle (MAV) in the future.
Keywords :
acoustic noise; aeroacoustics; aerospace components; autonomous aerial vehicles; carbon fibres; elasticity; noise abatement; polymer films; MAV; PET; acoustic comparison; carbon fiber; edge spars; flapping frequency; flapping microair-vehicles; flapping wings; hyper-elastic latex film; latex wing; noise reduction; stealth microair-vehicle; stiffened ribs; wingspan; Aerodynamics; Films; Noise; Noise reduction; Positron emission tomography; Vehicles; Latex; micro-air-vehilce (MAV); noise reduction;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Nano/Micro Engineered and Molecular Systems (NEMS), 2015 IEEE 10th International Conference on
Type :
conf
DOI :
10.1109/NEMS.2015.7147403
Filename :
7147403
Link To Document :
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