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 6K AIRFOIL to GOE 133 (MVA H.11) AIRFOIL

Page 2 of 21     1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20     Next

(goe06k-il) GOE 6K AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 6K AIRFOILGottingen 6K airfoil
Max thickness 7.5% at 50% chord
Max camber 3.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe07k-il) GOE 7K AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 7K AIRFOILGottingen 7K airfoil
Max thickness 11% at 50% chord
Max camber 4.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe08k-il) GOE 8K AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 8K AIRFOILGottingen 8K airfoil
Max thickness 14.9% at 50% chord
Max camber 6.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe09k-il) GOE 9K AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 9K AIRFOILGottingen 9K airfoil
Max thickness 2.5% at 50% chord
Max camber 0.9% at 60% chord
Source UIUC Airfoil Coordinates Database

(goe100-il) GOE 100 (SOPWITH) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 100 (SOPWITH) AIRFOILGottingen 100 (Sopwith) airfoil
Max thickness 6.6% at 20% chord
Max camber 3.6% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe101-il) GOE 101 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 101 AIRFOILGottingen 101 airfoil
Max thickness 6.9% at 30% chord
Max camber 4% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe10k-il) GOE 10K AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 10K AIRFOILGottingen 10K airfoil
Max thickness 3.9% at 50% chord
Max camber 1.4% at 60% chord
Source UIUC Airfoil Coordinates Database

(goe113-il) GOE 113 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 113 AIRFOILGottingen 113 airfoil
Max thickness 6.7% at 30% chord
Max camber 3% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe114-il) GOE 114 (MVA MK.1) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 114 (MVA MK.1) AIRFOILGottingen 114 (MVA MK.1) airfoil
Max thickness 9.6% at 29.7% chord
Max camber 3.5% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe115-il) GOE 115 (MVA MK.2) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 115 (MVA MK.2) AIRFOILGottingen 115 (MVA MK.2) airfoil
Max thickness 9.7% at 29.7% chord
Max camber 3.7% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe116-il) GOE 116 (MVA MK.3) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 116 (MVA MK.3) AIRFOILGottingen 116 (MVA MK.3) airfoil
Max thickness 9.3% at 39.8% chord
Max camber 4.1% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe117-il) GOE 117 (MVA MK.4) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 117 (MVA MK.4) AIRFOILGottingen 117 (MVA MK.4) airfoil
Max thickness 9% at 29.8% chord
Max camber 4.6% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe118-il) GOE 118 (MVA MK.7) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 118 (MVA MK.7) AIRFOILGottingen 118 (MVA MK.7) airfoil
Max thickness 8.6% at 29.9% chord
Max camber 5.7% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe11k-il) GOE 11K AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 11K AIRFOILGottingen 11K airfoil
Max thickness 7.5% at 50% chord
Max camber 2.7% at 60% chord
Source UIUC Airfoil Coordinates Database

(goe121-il) GOE 121 (MVA H.1) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 121 (MVA H.1) AIRFOILGottingen 121 (MVA H.1) airfoil
Max thickness 6.7% at 19.9% chord
Max camber 4.6% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe122-il) GOE 122 (MVA H.2) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 122 (MVA H.2) AIRFOILGottingen 122 (MVA H.2) airfoil
Max thickness 7.3% at 30% chord
Max camber 4.1% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe123-il) GOE 123 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 123 AIRFOILGottingen 123 airfoil
Max thickness 5.4% at 25% chord
Max camber 5.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe124-il) GOE 124 (MVA H.4) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 124 (MVA H.4) AIRFOILGottingen 124 (MVA H.4) airfoil
Max thickness 7.9% at 29.9% chord
Max camber 5.6% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe12k-il) GOE 12K AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 12K AIRFOILGottingen 12K airfoil
Max thickness 11.1% at 50% chord
Max camber 4.1% at 60% chord
Source UIUC Airfoil Coordinates Database

(goe133-il) GOE 133 (MVA H.11) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 133 (MVA H.11) AIRFOILGottingen 133 (MVA H.11) airfoil
Max thickness 7.9% at 30% chord
Max camber 4.3% at 30% chord
Source UIUC Airfoil Coordinates Database
Page 2 of 21     1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20     Next

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