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 177 AIRFOIL to GOE 228 (MVA H.38) AIRFOIL

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

(goe177-il) GOE 177 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 177 AIRFOILGottingen 177 airfoil
Max thickness 7.7% at 20% chord
Max camber 5% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe178-il) GOE 178 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 178 AIRFOILGottingen 178 airfoil
Max thickness 8.5% at 30% chord
Max camber 4.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe180-il) GOE 180 (MVA H.26) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 180 (MVA H.26) AIRFOILGottingen 180 (MVA H.26) airfoil
Max thickness 8.7% at 30% chord
Max camber 4.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe182-il) GOE 182 (MVA H.27) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 182 (MVA H.27) AIRFOILGottingen 182 (MVA H.27) airfoil
Max thickness 9.5% at 19.9% chord
Max camber 5.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe184-il) GOE 184 (MVA H.29) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 184 (MVA H.29) AIRFOILGottingen 184 (MVA H.29) airfoil
Max thickness 8.3% at 19.9% chord
Max camber 5.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe187-il) GOE 187 (SCHTTE-LANZ 2U10) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 187 (SCHTTE-LANZ 2U10) AIRFOILGottingen 187 (Schatte-Lanz 2U10) airfoil
Max thickness 8.3% at 30% chord
Max camber 4.8% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe188-il) GOE 188 (SCHTTE-LANZ 3U10) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 188 (SCHTTE-LANZ 3U10) AIRFOILGottingen 188 (Schatte-Lanz 3U10) airfoil
Max thickness 8.9% at 30% chord
Max camber 4.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe190-il) GOE 190 (MVA MK.18) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 190 (MVA MK.18) AIRFOILGottingen 190 (MVA MK.18) airfoil
Max thickness 12.7% at 19.7% chord
Max camber 5.9% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe195-il) GOE 195 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 195 AIRFOILGottingen 195 airfoil
Max thickness 8.6% at 20% chord
Max camber 5.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe198-il) GOE 198 (L.F.G. 5294) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 198 (L.F.G. 5294) AIRFOILGottingen 198 (L.F.G. 5294) airfoil
Max thickness 7.8% at 19.9% chord
Max camber 6.5% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe199-il) GOE 199 (L.F.G. 5406) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 199 (L.F.G. 5406) AIRFOILGottingen 199 (L.F.G. 5406) airfoil
Max thickness 7.3% at 30% chord
Max camber 5.2% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe207-il) GOE 207 (AVIATIK V8) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 207 (AVIATIK V8) AIRFOILGottingen 207 (AVIATIK V8) airfoil
Max thickness 8.8% at 19.9% chord
Max camber 6.6% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe210-il) GOE 210 (DAIMLER) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 210 (DAIMLER) AIRFOILGottingen 210 (DAIMLER) airfoil
Max thickness 6.6% at 30% chord
Max camber 4.3% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe217-il) GOE 217 (MVA MK.12) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 217 (MVA MK.12) AIRFOILGottingen 217 (MVA MK.12) airfoil
Max thickness 19% at 29.2% chord
Max camber 6.3% at 59.4% chord
Source UIUC Airfoil Coordinates Database

(goe222-il) GOE 222 (MVA H.33) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 222 (MVA H.33) AIRFOILGottingen 222 (MVA H.33) airfoil
Max thickness 18.5% at 29.2% chord
Max camber 7.2% at 49.2% chord
Source UIUC Airfoil Coordinates Database

(goe223-il) GOE 223 (MVA H.34) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 223 (MVA H.34) AIRFOILGottingen 223 (MVA H.34) airfoil
Max thickness 18.8% at 29.1% chord
Max camber 5.7% at 49.1% chord
Source UIUC Airfoil Coordinates Database

(goe225-il) GOE 225 (MVA H.35) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 225 (MVA H.35) AIRFOILGottingen 225 (MVA H.35) airfoil
Max thickness 12.8% at 19.7% chord
Max camber 7.6% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe226-il) GOE 226 (MVA H.36) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 226 (MVA H.36) AIRFOILGottingen 226 (MVA H.36) airfoil
Max thickness 13.9% at 19.7% chord
Max camber 8.1% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe227-il) GOE 227 (MVA H.37) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 227 (MVA H.37) AIRFOILGottingen 227 (MVA H.37) airfoil
Max thickness 14.6% at 25% chord
Max camber 7.8% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe228-il) GOE 228 (MVA H.38) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 228 (MVA H.38) AIRFOILGottingen 228 (MVA H.38) airfoil
Max thickness 17.9% at 29.4% chord
Max camber 7% at 49.4% chord
Source UIUC Airfoil Coordinates Database
Page 4 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.