(e1098-il) EPPLER 1098 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1098 general aviation airfoil
Max thickness 18.9% at 36.6% chord
Max camber 3.7% at 54.5% chord
Source UIUC Airfoil Coordinates Database
|
(e1200-il) EPPLER 1200 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1200 general aviation airfoil
Max thickness 16.9% at 36.1% chord
Max camber 3.5% at 50.2% chord
Source UIUC Airfoil Coordinates Database
|
(e1210-il) EPPLER 1210 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1210 general aviation airfoil
Max thickness 15.9% at 21.1% chord
Max camber 5.2% at 33.3% chord
Source UIUC Airfoil Coordinates Database
|
(e1211-il) EPPLER 1211 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1211 general aviation airfoil
Max thickness 18% at 20.9% chord
Max camber 4.4% at 37.7% chord
Source UIUC Airfoil Coordinates Database
|
(e1212-il) EPPLER E1212 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1212 general aviation airfoil
Max thickness 17.7% at 23.4% chord
Max camber 3.2% at 36.4% chord
Source UIUC Airfoil Coordinates Database
|
|
(e1212mod-il) EPPLER E1212MOD AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1212 general aviation airfoil (as modified for use as Quickie wing airfoil)
Max thickness 17.7% at 20.1% chord
Max camber 2.6% at 35.1% chord
Source UIUC Airfoil Coordinates Database
|
(e1213-il) EPPLER 1213 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1213 general aviation airfoil
Max thickness 17.4% at 22.1% chord
Max camber 2.1% at 35.1% chord
Source UIUC Airfoil Coordinates Database
|
(e1214-il) EPPLER 1214 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1214 general aviation airfoil
Max thickness 19.8% at 26.2% chord
Max camber 2.1% at 30.4% chord
Source UIUC Airfoil Coordinates Database
|
(e1230-il) EPPLER 1230 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1230 general aviation airfoil (Long-EZ and Defiant wing airfoil)
Max thickness 17.4% at 30.9% chord
Max camber 3.6% at 25.6% chord
Source UIUC Airfoil Coordinates Database
|
(e1233-il) EPPLER 1233 AIRFOIL | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E1233 general aviation airfoil
Max thickness 18.9% at 29.8% chord
Max camber 4.4% at 29.8% chord
Source UIUC Airfoil Coordinates Database
|
(e168-il) E168 (12.45%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E168 low Reynolds number airfoil
Max thickness 12.4% at 26.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
|
(e169-il) E169 (14.4%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E169 low Reynolds number airfoil
Max thickness 14.4% at 26.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
|
(e171-il) (Dicke 12.28%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E171 low Reynolds number airfoil
Max thickness 12.3% at 32.4% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
|
|
(e174-il) E174 (Dicke 8.92%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E174 low Reynolds number airfoil
Max thickness 8.9% at 31.2% chord
Max camber 3.3% at 44.9% chord
Source UIUC Airfoil Coordinates Database
|
(e176-il) E176 (8.83%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E176 low Reynolds number airfoil
Max thickness 8.8% at 30.5% chord
Max camber 2.9% at 44.2% chord
Source UIUC Airfoil Coordinates Database
|
(e178-il) E178 (8.69%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E178 low Reynolds number airfoil
Max thickness 8.7% at 29.8% chord
Max camber 2.8% at 38.8% chord
Source UIUC Airfoil Coordinates Database
|
(e180-il) E180 (8.59%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E180 low Reynolds number airfoil
Max thickness 8.6% at 33.5% chord
Max camber 2% at 38.1% chord
Source UIUC Airfoil Coordinates Database
|
(e182-il) E182 (8.47%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E182 low Reynolds number airfoil
Max thickness 8.5% at 32.4% chord
Max camber 1.2% at 37.5% chord
Source UIUC Airfoil Coordinates Database
|
(e184-il) E184 (8.33%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E184 low Reynolds number airfoil
Max thickness 8.3% at 33.3% chord
Max camber 0.8% at 38.3% chord
Source UIUC Airfoil Coordinates Database
|
(e186-il) E186 (10.27%) | Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
|
 | Eppler E186 low Reynolds number airfoil
Max thickness 10.2% at 29% chord
Max camber 0.8% at 29% chord
Source UIUC Airfoil Coordinates Database
|
