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Curvas Polares de Perfiles de Aire Eppler, Selig y Liebeck

This document summarizes polar curve data from three different airfoil profiles - Eppler E423, Selig S1223, and Liebeck - tested over a range of Reynolds numbers and Mach numbers. The data was obtained from wind tunnel measurements conducted by the Low-Speed Airfoils Tests (LSATs) group at the University of Illinois Urbana-Champaign led by Dr. Selig.

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Vany Braun
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29 views3 pages

Curvas Polares de Perfiles de Aire Eppler, Selig y Liebeck

This document summarizes polar curve data from three different airfoil profiles - Eppler E423, Selig S1223, and Liebeck - tested over a range of Reynolds numbers and Mach numbers. The data was obtained from wind tunnel measurements conducted by the Low-Speed Airfoils Tests (LSATs) group at the University of Illinois Urbana-Champaign led by Dr. Selig.

Uploaded by

Vany Braun
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
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Apéndice B

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_

Curvas polares de los perfiles Eppler, Selig y Liebeck.

Eppler E423(Re=99700-300800,UIUC,Show Data)


Reynolds
99700-300800 Mach Number-------
Number
The source:M.S.Selig,C.A.Lyon,P.Giguere,C.Ninham and J.J.Guglielmo,"Summary of
Comment
Low-Speed Airfoil Data, Volume 2"
Registrant Hiroshi Takeuchi
Obtained from Wind Tunnel measurement
The group
UIUC LSATs(Selig group)
tested by

120
Selig S1223(Re=100600-249700,UIUC,Show Data)
Reynolds
100600-249700 Mach Number-----
Number
The source:M.S.Selig,J.J.Guglielmo,A.P.Broeren and P.Giguere,"Summary of Low-Speed Airfoil
Comment
Data, Volume 1"
Registrant Hiroshi Takeuchi
Obtained from Wind Tunnel measurement
The group tested
UIUC LSATs(Selig group)
by

121
Liebeck (Re=59500-298700,UIUC,Show Data)
Reynolds
59500-298700 Mach Number---
Number
The source:C.A.Lyon,P.Broeren,P.Giguere,A.Gopalarathnam and M.S.Selig,"Summary of Low-
Comment
Speed Airfoil Data, Volume 3"
Registrant Hiroshi Takeuchi
Obtained from Wind Tunnel measurement
The group
UIUC LSATs(Selig group)
tested by

122

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