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 (G).

GOE 611 AIRFOIL to GOE 632 AIRFOIL

Page 18 of 21     2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21     Next

(goe611-il) GOE 611 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 611 AIRFOILGottingen 611 airfoil
Max thickness 12.9% at 29.9% chord
Max camber 5.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe612-il) GOE 612 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 612 AIRFOILGottingen 612 airfoil
Max thickness 15% at 29.5% chord
Max camber 5% at 49.5% chord
Source UIUC Airfoil Coordinates Database

(goe613-il) GOE 613 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 613 AIRFOILGottingen 613 airfoil
Max thickness 10.3% at 30% chord
Max camber 4.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe614-il) GOE 614 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 614 AIRFOILGottingen 614 airfoil
Max thickness 18.8% at 29.2% chord
Max camber 6.2% at 39.2% chord
Source UIUC Airfoil Coordinates Database

(goe615-il) GOE 615 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 615 AIRFOILGottingen 615 airfoil
Max thickness 13.7% at 29.7% chord
Max camber 5.6% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe617-il) GOE 617 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 617 AIRFOILGottingen 617 airfoil
Max thickness 13.9% at 30% chord
Max camber 2.2% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe619-il) GOE 619 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 619 AIRFOILGottingen 619 airfoil
Max thickness 13.7% at 19.5% chord
Max camber 4.5% at 49.5% chord
Source UIUC Airfoil Coordinates Database

(goe620-il) GOE 620 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 620 AIRFOILGottingen 620 airfoil
Max thickness 17.5% at 30% chord
Max camber 5.9% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe621-il) GOE 621 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 621 AIRFOILGottingen 621 airfoil
Max thickness 15% at 29.5% chord
Max camber 5% at 49.5% chord
Source UIUC Airfoil Coordinates Database

(goe622-il) GOE 622 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 622 AIRFOILGottingen 622 airfoil
Max thickness 8% at 30% chord
Max camber 2.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe623-il) GOE 623 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 623 AIRFOILGottingen 623 airfoil
Max thickness 12% at 30% chord
Max camber 3.8% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe624-il) GOE 624 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 624 AIRFOILGottingen 624 airfoil
Max thickness 16% at 30% chord
Max camber 5.2% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe625-il) GOE 625 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 625 AIRFOILGottingen 625 airfoil
Max thickness 20% at 30% chord
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe626-il) GOE 626 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 626 AIRFOILGottingen 626 airfoil
Max thickness 16.5% at 19.3% chord
Max camber 5.1% at 49.3% chord
Source UIUC Airfoil Coordinates Database

(goe627-il) GOE 627 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 627 AIRFOILGottingen 627 airfoil
Max thickness 15.8% at 30% chord
Max camber 4.1% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe628-il) GOE 628 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 628 AIRFOILGottingen 628 airfoil
Max thickness 16.7% at 19.4% chord
Max camber 5.6% at 39.3% chord
Source UIUC Airfoil Coordinates Database

(goe629-il) GOE 629 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 629 AIRFOILGottingen 629 airfoil
Max thickness 13.6% at 29.4% chord
Max camber 2.8% at 39.4% chord
Source UIUC Airfoil Coordinates Database

(goe63-il) GOE 63 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 63 AIRFOILGottingen 63 airfoil
Max thickness 8.3% at 19.9% chord
Max camber 6.7% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe630-il) GOE 630 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 630 AIRFOILGottingen 630 airfoil
Max thickness 12.6% at 29.8% chord
Max camber 7.7% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe632-il) GOE 632 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 632 AIRFOILGottingen 632 airfoil
Max thickness 14% at 30% chord
Max camber 3.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Page 18 of 21     2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21     Next

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