Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

Airfoil database list (E).

EPPLER 485 AIRFOIL to EPPLER 554 AIRFOIL

Page 6 of 11     1 2 3 4 5 6 7 8 9 10 11     Next

(e485-il) EPPLER 485 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 485 AIRFOILEppler E485 tailplane airfoil
Max thickness 12.5% at 31.8% chord
Max camber 1.1% at 27.1% chord
Source UIUC Airfoil Coordinates Database

(e49-il) EPPLER 49 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 49 AIRFOILEppler E49 low Reynolds number airfoil
Max thickness 7.2% at 38.4% chord
Max camber 6.5% at 62.2% chord
Source UIUC Airfoil Coordinates Database

(e502-il) EPPLER 502 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 502 AIRFOILEppler E502 general purpose airfoil
Max thickness 15.6% at 42.1% chord
Max camber 1.5% at 32.3% chord
Source UIUC Airfoil Coordinates Database

(e520-il) EPPLER 520 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 520 AIRFOILEppler E520 tailplane airfoil
Max thickness 15% at 36.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e521-il) EPPLER 521 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 521 AIRFOILEppler E521 tailplane airfoil
Max thickness 13.8% at 37% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e540-il) EPPLER 540 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 540 AIRFOILEppler E540 general aviation airfoil
Max thickness 16.9% at 45.5% chord
Max camber 1.6% at 35.7% chord
Source UIUC Airfoil Coordinates Database

(e541-il) EPPLER 541 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 541 AIRFOILEppler E541 general aviation airfoil
Max thickness 16.6% at 46.2% chord
Max camber 1.7% at 36.3% chord
Source UIUC Airfoil Coordinates Database

(e542-il) EPPLER 542 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 542 AIRFOILEppler E542 general aviation airfoil
Max thickness 16.9% at 41.3% chord
Max camber 1.9% at 31.5% chord
Source UIUC Airfoil Coordinates Database

(e543-il) EPPLER 543 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 543 AIRFOILEppler E543 general aviation airfoil
Max thickness 17.2% at 40.7% chord
Max camber 1.9% at 31% chord
Source UIUC Airfoil Coordinates Database

(e544-il) EPPLER 544 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 544 AIRFOILEppler E544 general aviation airfoil
Max thickness 17.5% at 40% chord
Max camber 1.9% at 30.5% chord
Source UIUC Airfoil Coordinates Database

(e545-il) EPPLER 545 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 545 AIRFOILEppler E545 general aviation airfoil
Max thickness 17.4% at 39.3% chord
Max camber 1.8% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(e546-il) EPPLER 546 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 546 AIRFOILEppler E546 general aviation airfoil
Max thickness 16.2% at 40.3% chord
Max camber 1.8% at 26.2% chord
Source UIUC Airfoil Coordinates Database

(e547-il) EPPLER 547 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 547 AIRFOILEppler E547 general aviation airfoil
Max thickness 17.4% at 40.3% chord
Max camber 2% at 30.7% chord
Source UIUC Airfoil Coordinates Database

(e548-il) EPPLER 548 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 548 AIRFOILEppler E548 general aviation airfoil
Max thickness 17.4% at 35.4% chord
Max camber 2.2% at 26.1% chord
Source UIUC Airfoil Coordinates Database

(e549-il) EPPLER 549 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 549 AIRFOILEppler E549 general aviation airfoil
Max thickness 18.1% at 38.7% chord
Max camber 2% at 34% chord
Source UIUC Airfoil Coordinates Database

(e550-il) EPPLER 550 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 550 AIRFOILEppler E550 general aviation airfoil
Max thickness 18.2% at 34% chord
Max camber 2.2% at 29.4% chord
Source UIUC Airfoil Coordinates Database

(e551-il) EPPLER 551 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 551 AIRFOILEppler E551 general aviation airfoil
Max thickness 18.2% at 32.4% chord
Max camber 2.8% at 57.1% chord
Source UIUC Airfoil Coordinates Database

(e552-il) EPPLER 552 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 552 AIRFOILEppler E552 general aviation airfoil
Max thickness 18.4% at 32.4% chord
Max camber 2.6% at 51.8% chord
Source UIUC Airfoil Coordinates Database

(e553-il) EPPLER 553 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 553 AIRFOILEppler E553 general aviation airfoil
Max thickness 18.1% at 31.8% chord
Max camber 2.9% at 56.6% chord
Source UIUC Airfoil Coordinates Database

(e554-il) EPPLER 554 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 554 AIRFOILEppler E554 general aviation airfoil
Max thickness 18.2% at 31.8% chord
Max camber 2.7% at 56.6% chord
Source UIUC Airfoil Coordinates Database
Page 6 of 11     1 2 3 4 5 6 7 8 9 10 11     Next

Please see the source web site or designer for any license conditions.