Aerodynamic Analysis of Open Trailing Edge Airfoils at Low Reynolds Number
| Data(s) |
2011
|
|---|---|
| Resumo |
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 |
| Formato |
application/pdf |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
E.T.S.I. Aeronáuticos (UPM) |
| Relação |
http://oa.upm.es/13564/1/INVE_MEM_2011_114588.pdf https://www.aiaa.org/ProceedingsDetail.aspx?id=3778 info:eu-repo/semantics/altIdentifier/doi/null |
| Direitos |
http://creativecommons.org/licenses/by-nc-nd/3.0/es/ info:eu-repo/semantics/openAccess |
| Fonte |
Proceedings of 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition | 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition | 04/01/2011 - 07/01/2011 | Orlando, Florida, USA |
| Palavras-Chave | #Aeronáutica #Física |
| Tipo |
info:eu-repo/semantics/conferenceObject Ponencia en Congreso o Jornada PeerReviewed |
