Low-noise flapping wings with tensed membrane

Date

2020-04-15

Supervisor/s

Journal Title

Journal ISSN

Volume Title

Publisher

AIAA

Department

Type

Article

ISSN

0001-1452

Format

Free to read from

Citation

Debiasi M, Lu Z, Nguyen QV, Chan WL. (2020) Low-noise flapping wings with tensed membrane. AIAA Journal, Volume 58, Issue 6, June 2020, pp. 2388-2397

Abstract

Micro air vehicles with flapping wings have the potential to be both more efficient and maneuverable than similar-sized fixed- or rotary-wing aircraft. Reducing the perceived noise produced by flapping wings without compromising or possibly enhancing their aerodynamic performance would be crucial in surveillance and military applications. To this aim, flapping wings have been designed and fabricated for which the supporting stiffeners tense the Mylar membrane to which they are bonded. The sound produced by these wings at different flapping frequencies has been recorded in an anechoic chamber simultaneously to the upward thrust they create. Comparing their characteristics and performance with those of flapping wings of conventional design suggests that tensing the wing’s membrane can increase the thrust while decreasing the typical rustling noise of the flapping wings

Description

Software Description

Software Language

Github

Keywords

Sound measurements, Noise reduction, Micro Air Vehicle, Flapping wing

DOI

Rights

Attribution-NonCommercial 4.0 International

Relationships

Relationships

Supplements

Funder/s