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Airfoil database list (E).

EPPLER 856 AIRFOIL to EH 2.0/12

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(e856-il) EPPLER 856 AIRFOIL

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EPPLER 856 AIRFOILEppler E856 propeller airfoil
Max thickness 18.2% at 31.9% chord
Max camber 4.2% at 50.2% chord
Source UIUC Airfoil Coordinates Database

(e857-il) EPPLER 857 AIRFOIL

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EPPLER 857 AIRFOILEppler E857 propeller airfoil
Max thickness 20.3% at 31.5% chord
Max camber 4.9% at 45.1% chord
Source UIUC Airfoil Coordinates Database

(e858-il) EPPLER 858 AIRFOIL

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EPPLER 858 AIRFOILEppler E858 propeller airfoil
Max thickness 22.7% at 26.6% chord
Max camber 4.7% at 44.3% chord
Source UIUC Airfoil Coordinates Database

(e862-il) EPPLER 862 STRUT AIRFOIL

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EPPLER 862 STRUT AIRFOILEppler E862 strut airfoil
Max thickness 32.4% at 28.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e863-il) EPPLER 863 STRUT AIRFOIL

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EPPLER 863 STRUT AIRFOILEppler E863 strut airfoil
Max thickness 35.7% at 28.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e864-il) EPPLER 864 STRUT AIRFOIL

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EPPLER 864 STRUT AIRFOILEppler E864 strut airfoil
Max thickness 38.8% at 32.7% chord
Max camber 0.1% at 10.8% chord
Source UIUC Airfoil Coordinates Database

(e874-il) EPPLER 874 HYDROFOIL AIRFOIL

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EPPLER 874 HYDROFOIL AIRFOILEppler E874 hydrofoil
Max thickness 7.9% at 28.8% chord
Max camber 0.9% at 35.7% chord
Source UIUC Airfoil Coordinates Database

(e904-il) EPPLER 904 AIRFOIL

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EPPLER 904 AIRFOILEppler E904 hydrofoil
Max thickness 9% at 44.9% chord
Max camber 1.3% at 50.4% chord
Source UIUC Airfoil Coordinates Database

(e908-il) EPPLER 908 AIRFOIL

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EPPLER 908 AIRFOILEppler E908 hydrofoil
Max thickness 9% at 44.8% chord
Max camber 2.8% at 66.3% chord
Source UIUC Airfoil Coordinates Database

(ea61009-il) EPPLER EA 6(-1)-009 AIRFOIL

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EPPLER EA 6(-1)-009 AIRFOILEppler EA 6(-1)-009 airfoil
Max thickness 9% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ea61012-il) EPPLER EA 6(-1)-012 AIRFOIL

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EPPLER EA 6(-1)-012 AIRFOILEppler EA 6(-1)-012 airfoil
Max thickness 12% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ea81006-il) EPPLER EA 8(-1)-006 AIRFOIL

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EPPLER EA 8(-1)-006 AIRFOILEppler EA 8(-1)-006 airfoil
Max thickness 6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ebambino7-il) E. Bambino

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E. BambinoE. Bambino airfoil
Max thickness 6% at 40% chord
Max camber 1.9% at 20% chord
Source UIUC Airfoil Coordinates Database

(ec863914-il) EPPLER EC 86(-3)-914 AIRFOIL

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EPPLER EC 86(-3)-914 AIRFOILEppler EC 86(-3)-914 airfoil
Max thickness 14.3% at 35.5% chord
Max camber 4.4% at 71.2% chord
Source UIUC Airfoil Coordinates Database

(eh0009-il) EH 0.0/9.0

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EH 0.0/9.0John Yost EH 0.0/9.0 for tailless R/C aircraft
Max thickness 9% at 28.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(eh1070-il) Eh 1.0/7.0

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Eh 1.0/7.0John Yost EH 1.0/7.0 for tailless R/C aircraft
Max thickness 7% at 28.7% chord
Max camber 1% at 25.9% chord
Source UIUC Airfoil Coordinates Database

(eh1090-il) EH 1.0/9.0

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EH 1.0/9.0John Yost EH 1.0/9.0 for tailless R/C aircraft
Max thickness 9% at 28.7% chord
Max camber 1% at 25.9% chord
Source UIUC Airfoil Coordinates Database

(eh1590-il) EH 1.5/9.0

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EH 1.5/9.0John Yost EH 1.5/9.0 for tailless R/C aircraft
Max thickness 9% at 28.7% chord
Max camber 1.5% at 25.9% chord
Source UIUC Airfoil Coordinates Database

(eh2010-il) EH 2.0/10

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EH 2.0/10John Yost EH 2.0/10 for tailless R/C aircraft
Max thickness 10.1% at 28.7% chord
Max camber 2% at 25.9% chord
Source UIUC Airfoil Coordinates Database

(eh2012-il) EH 2.0/12

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EH 2.0/12John Yost EH 2.0/12 for tailless R/C aircraft
Max thickness 12% at 28.7% chord
Max camber 2% at 25.9% chord
Source UIUC Airfoil Coordinates Database
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