| Full text | |
| Author(s): |
Total Authors: 2
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| Affiliation: | [1] Univ Sao Paulo, Sao Carlos Sch Engn, Sao Carlos - Brazil
Total Affiliations: 1
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| Document type: | Journal article |
| Source: | MECCANICA; v. 56, n. 11 JUL 2021. |
| Web of Science Citations: | 0 |
| Abstract | |
Technologies inspired by the functioning and behavior of biological beings are commonly developed for aircraft flight. Among the bio-inspired approaches that have grown in interest, particularly for unmanned aerial vehicle flight, is based on the behavior of bird's cover feathers under higher angles of attack. The covert feathers, when activated by separated flows, promote lift increment that helps in certain maneuvers. This work investigates the benefit in the stall and post-stall performance of employing bio-inspired covert feathers devices attached to an airfoil's upper surface. To fill the gaps in the recent technical literature, experimental analysis of an SD7003 airfoil was executed in a wind tunnel with the application of bio-inspired covert feathers of different shapes and tapes in three chordwise positions. The bio-inspired devices were conceived to resemble the feathers' lightness and discrete-distribution along with the wing model. Experiments were carried out measuring the aerodynamic forces and moment at Reynolds number around 170,000 for static and dynamic ramp-up and hold pitching motion. It has been confirmed that the use of bio-inspired covert feathers brought benefits to the stall and post-stall behavior of the airfoil. The maximum lift has increased, and the transition from attached to stalled flow around the airfoil tends to be smoother when the devices were used. Four shapes for the bio-inspired devices and three positions in chordwise direction were considered. The best performance among the case was encountered for a jagged bio-inspired device taped at a quarter-chord position. Indeed, the most forward position for all the devices resulted in higher maximum lift and increment to the respective angle of attack. Ramp-up and hold wind tunnel tests also confirmed the best performance of jagged bio-inspired devices nearer the leading edge. The aerodynamic response to the pitching motion showed that the stall and post-stall regime occur much smoother, indicating that the approach presents good potential for dynamic stall or gust response passive control. (AU) | |
| FAPESP's process: | 17/02926-9 - Airfoil unsteady aerodynamic loading assessment under dynamic stall for semi-empirical model validation |
| Grantee: | Flávio Donizeti Marques |
| Support Opportunities: | Regular Research Grants |