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Cárdenas Rondón, J.A., Ogueta Gutiérrez, Mikel ORCID: https://orcid.org/0000-0001-9183-450X and Franchini Longhi, Sebastian Nicolas
ORCID: https://orcid.org/0000-0002-1476-9174
(2019).
Experimental study of the effect of the reduced frequency in the airfoil's aerodynamic characteristics.
In: "8th European Conference for Aeronautics and Space Sciences", 1-4 Jul, Madrid.
https://doi.org/10.13009/EUCASS2019-449.
Title: | Experimental study of the effect of the reduced frequency in the airfoil's aerodynamic characteristics |
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Author/s: |
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Item Type: | Presentation at Congress or Conference (Article) |
Event Title: | 8th European Conference for Aeronautics and Space Sciences |
Event Dates: | 1-4 Jul |
Event Location: | Madrid |
Title of Book: | 8th European Conference for Aeronautics and Space Science EUCASS 2019 |
Date: | July 2019 |
Subjects: | |
Faculty: | Instituto de Microgravedad Ignacio Da Riva (UPM) |
Department: | Aeronaves y Vehículos Espaciales |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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The aim of this research is to describe a dynamic system developed to analyse the characteristics of airfoils immersed in an unsteady flow, being able to reproduce different movement including coupled bending and torsion. Using an airfoil model with pressure taps, NACA 0015 was analysed in two cases: bending motion and flutter, both with a reduced frequency of 0.086. The hysteresis loops of both cases are presented. An outstanding different of c1 and cd was observed depending on whether the effective angle of attack was increased or decreased. The need to create a catalogue of airfoils in unsteady regime is revealed.
Item ID: | 65203 |
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DC Identifier: | https://oa.upm.es/65203/ |
OAI Identifier: | oai:oa.upm.es:65203 |
DOI: | 10.13009/EUCASS2019-449 |
Official URL: | https://eucass.eu/9-news/79-eucass-2019-dois-of-fu... |
Deposited by: | Memoria Investigacion |
Deposited on: | 16 Feb 2021 11:14 |
Last Modified: | 16 Feb 2021 11:14 |