Full text
Preview |
PDF
- Requires a PDF viewer, such as GSview, Xpdf or Adobe Acrobat Reader
Download (1MB) | Preview |
Aerodynamic Study of Airfoils with Leading Edge Imperfections at Low Reynolds Number
Citation
Ayuso Moreno, Luis Manuel 
ORCID: https://orcid.org/0000-0002-5463-2156, Sant Palma, Rodolfo ORCID: https://orcid.org/0000-0002-3396-5963 and Meseguer Ruiz, José
(2010).
Aerodynamic Study of Airfoils with Leading Edge Imperfections at Low Reynolds Number.
In: "40th Fluid Dynamics Conference and Exhibit", 28/06/2010 - 01/07/2010, Chicago, Illinois, USA. pp. 1-10.
Description
| Title: | Aerodynamic Study of Airfoils with Leading Edge Imperfections at Low Reynolds Number |
|---|---|
| Author/s: |
|
| Item Type: | Presentation at Congress or Conference (Article) |
| Event Title: | 40th Fluid Dynamics Conference and Exhibit |
| Event Dates: | 28/06/2010 - 01/07/2010 |
| Event Location: | Chicago, Illinois, USA |
| Title of Book: | 40th AIAA Fluid Dynamics Conference proceedings |
| Date: | 28 June 2010 |
| Subjects: | |
| Faculty: | E.U.I.T. Aeronáutica (UPM) |
| Department: | Aerotecnia [hasta 2014] |
| Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
Abstract
A study has been made on the influence of the leading edge imperfections in airfoils used in different devices relating their aerodynamic performances. Wind tunnel tests have been made at different Reynolds numbers and angle of attacks in order to show this effect. Later, a quantitative study of the aerodynamic properties has been made based on the different leading edge imperfections and their size.
More information
| Item ID: | 32240 |
|---|---|
| DC Identifier: | https://oa.upm.es/32240/ |
| OAI Identifier: | oai:oa.upm.es:32240 |
| Deposited by: | Memoria Investigacion |
| Deposited on: | 10 Oct 2014 13:07 |
| Last Modified: | 10 Feb 2023 08:55 |
