Aerodynamic Study of Airfoils with Leading Edge Imperfections at Low Reynolds Number

Ayuso Moreno, Luis Manuel and Sant Palma, Rodolfo 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:
  • Ayuso Moreno, Luis Manuel
  • Sant Palma, Rodolfo
  • Meseguer Ruiz, José
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

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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: http://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 Oct 2014 13:07
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