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Aerodynamic Analysis of Open Trailing Edge Airfoils at Low Reynolds Number
Citation
Sant Palma, Rodolfo and Ayuso Moreno, Luis Manuel and Meseguer Ruiz, José (2011). Aerodynamic Analysis of Open Trailing Edge Airfoils at Low Reynolds Number. In: "49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition", 04/01/2011 - 07/01/2011, Orlando, Florida, USA. pp. 1-10.
Description
| Title: | Aerodynamic Analysis of Open Trailing Edge Airfoils at Low Reynolds Number |
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| Author/s: |
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| Item Type: | Presentation at Congress or Conference (Article) |
| Event Title: | 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition |
| Event Dates: | 04/01/2011 - 07/01/2011 |
| Event Location: | Orlando, Florida, USA |
| Title of Book: | Proceedings of 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition |
| Date: | 2011 |
| Subjects: | |
| Faculty: | E.T.S.I. Aeronáuticos (UPM) |
| Department: | Vehículos Aeroespaciales [hasta 2014] |
| Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
Abstract
A study has been made on the influence of the open trailing edge in airfoils used in different devices relating their aerodynamic performances. Wind tunnel tests have been made at different Reynolds numbers and angles of attack in order to show this effect. Besides, a quantitative study of the aerodynamic properties has been made based on the different trailing edge thickness
More information
| Item ID: | 13564 |
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| DC Identifier: | https://oa.upm.es/13564/ |
| OAI Identifier: | oai:oa.upm.es:13564 |
| Official URL: | https://www.aiaa.org/ProceedingsDetail.aspx?id=3778 |
| Deposited by: | Memoria Investigacion |
| Deposited on: | 22 Nov 2012 10:01 |
| Last Modified: | 06 Oct 2014 14:32 |
