Aerodynamic Analysis of Open Trailing Edge Airfoils at Low Reynolds Number

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
Author/s:
  • Sant Palma, Rodolfo
  • Ayuso Moreno, Luis Manuel
  • Meseguer Ruiz, José
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

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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
DC Identifier: http://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
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