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 633 AIRFOIL to GOE 692 AIRFOIL

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

(goe633-il) GOE 633 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 633 AIRFOILGottingen 633 airfoil
Max thickness 13.8% at 19.7% chord
Max camber 4% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe645-il) GOE 645 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 645 AIRFOILGottingen 645 airfoil
Max thickness 15.4% at 19.4% chord
Max camber 4.8% at 39.4% chord
Source UIUC Airfoil Coordinates Database

(goe646-il) GOE 646 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 646 AIRFOILGottingen 646 airfoil
Max thickness 18.3% at 29% chord
Max camber 4.5% at 49% chord
Source UIUC Airfoil Coordinates Database

(goe647-il) GOE 647 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 647 AIRFOILGottingen 647 airfoil
Max thickness 16.2% at 19.5% chord
Max camber 5.3% at 39.4% chord
Source UIUC Airfoil Coordinates Database

(goe648-il) GOE 648 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 648 AIRFOILGottingen 648 airfoil
Max thickness 15.2% at 29.4% chord
Max camber 3.9% at 39.4% chord
Source UIUC Airfoil Coordinates Database

(goe650-il) GOE 650 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 650 AIRFOILGottingen 650 airfoil
Max thickness 13.4% at 19.5% chord
Max camber 4.4% at 49.5% chord
Source UIUC Airfoil Coordinates Database

(goe652-il) GOE 652 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 652 AIRFOILGottingen 652 airfoil
Max thickness 17.1% at 20% chord
Max camber 9.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe654-il) GOE 654 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 654 AIRFOILGottingen 654 airfoil
Max thickness 14.5% at 30% chord
Max camber 5.2% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe655-il) GOE 655 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 655 AIRFOILGottingen 655 airfoil
Max thickness 13.9% at 30% chord
Max camber 4.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe670-il) GOE 670 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 670 AIRFOILGottingen 670 airfoil
Max thickness 9% at 30% chord
Max camber 3.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe673-il) GOE 673 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 673 AIRFOILGottingen 673 airfoil
Max thickness 10.8% at 29.7% chord
Max camber 2.8% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe675-il) GOE 675 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 675 AIRFOILGottingen 675 airfoil
Max thickness 14.9% at 29.5% chord
Max camber 5.9% at 39.5% chord
Source UIUC Airfoil Coordinates Database

(goe676-il) GOE 676 (= M 12) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 676 (= M 12) AIRFOILGottingen 676 (= M 12) airfoil
Max thickness 11.9% at 30% chord
Max camber 2% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe677-il) GOE 677 (= M 6) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 677 (= M 6) AIRFOILGottingen 677 (= M 6) airfoil
Max thickness 12% at 30% chord
Max camber 2.2% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe679-il) GOE 679 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 679 AIRFOILGottingen 679 airfoil
Max thickness 18.3% at 29.1% chord
Max camber 4.5% at 39.1% chord
Source UIUC Airfoil Coordinates Database

(goe681-il) GOE 681 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 681 AIRFOILGottingen 681 airfoil
Max thickness 16.8% at 29.2% chord
Max camber 4.4% at 39.2% chord
Source UIUC Airfoil Coordinates Database

(goe682-il) GOE 682 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 682 AIRFOILGottingen 682 airfoil
Max thickness 10.7% at 30% chord
Max camber 4.3% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe683-il) GOE 683 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 683 AIRFOILGottingen 683 airfoil
Max thickness 19.9% at 30% chord
Max camber 3% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe685-il) GOE 685 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 685 AIRFOILGottingen 685 airfoil
Max thickness 13.1% at 19.6% chord
Max camber 4.2% at 49.5% chord
Source UIUC Airfoil Coordinates Database

(goe692-il) GOE 692 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 692 AIRFOILGottingen 692 airfoil
Max thickness 16.1% at 30% chord
Max camber 5% at 40% chord
Source UIUC Airfoil Coordinates Database
Page 19 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.