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 309 (MVA H.41) AIRFOIL to GOE 332 (PFALZ 61) AIRFOIL

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

(goe309-il) GOE 309 (MVA H.41) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 309 (MVA H.41) AIRFOILGottingen 309 (MVA H.41) airfoil
Max thickness 8.4% at 30% chord
Max camber 4.7% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe310-il) GOE 310 (MVA H.42) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 310 (MVA H.42) AIRFOILGottingen 310 (MVA H.42) airfoil
Max thickness 8.1% at 29.9% chord
Max camber 4.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe311-il) GOE 311 (MVA H.43) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 311 (MVA H.43) AIRFOILGottingen 311 (MVA H.43) airfoil
Max thickness 8.4% at 19.9% chord
Max camber 6.1% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe314-il) GOE 314 (HANSA-BRANDENBURG) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 314 (HANSA-BRANDENBURG) AIRFOILGottingen 314 (Hansa-Brandenburg) airfoil
Max thickness 8% at 29.9% chord
Max camber 4.7% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe315-il) GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 315 (HANSA-BRANDENBURG III.5) AIRFOILGottingen 315 (Hansa-Brandenburg III.5) airfoil
Max thickness 8.1% at 29.9% chord
Max camber 4.1% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe316-il) GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOILGottingen 316 (Hansa-Brandenburg IV.5) airfoil
Max thickness 9.1% at 29.9% chord
Max camber 4.2% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe318-il) GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOILGottingen 318 (Hansa-Brandenburg VI.5) airfoil
Max thickness 9.1% at 29.9% chord
Max camber 4.3% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe319-il) GOE 319 (HANSA-BRANDENBURG II) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 319 (HANSA-BRANDENBURG II) AIRFOILGottingen 319 (Hansa-Brandenburg II) airfoil
Max thickness 10.3% at 29.8% chord
Max camber 5.8% at 29.8% chord
Source UIUC Airfoil Coordinates Database

(goe320-il) GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 320 (HANSA-BRANDENBURG II.1) AIRFOILGottingen 320 (Hansa-Brandenburg II.1) airfoil
Max thickness 12.3% at 29.8% chord
Max camber 6.2% at 29.8% chord
Source UIUC Airfoil Coordinates Database

(goe321-il) GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 321 (HANSA-BRANDENBURG III.1) AIRFOILGottingen 321 (Hansa-Brandenburg III.1) airfoil
Max thickness 11.2% at 29.9% chord
Max camber 5.1% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe322-il) GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOILGottingen 322 (Hansa-Brandenburg IV.1) airfoil
Max thickness 13.1% at 29.8% chord
Max camber 6% at 29.8% chord
Source UIUC Airfoil Coordinates Database

(goe323-il) GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 323 (HANSA-BRANDENBURG V.1) AIRFOILGottingen 323 (Hansa-Brandenburg V.1) airfoil
Max thickness 11.1% at 29.8% chord
Max camber 5.2% at 29.8% chord
Source UIUC Airfoil Coordinates Database

(goe324-il) GOE 324 (HANSA-BRANDENBURG) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 324 (HANSA-BRANDENBURG) AIRFOILGottingen 324 (Hansa-Brandenburg) airfoil
Max thickness 13.1% at 29.8% chord
Max camber 5.9% at 29.8% chord
Source UIUC Airfoil Coordinates Database

(goe325-il) GOE 325 (PFALZ 54) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 325 (PFALZ 54) AIRFOILGottingen 325 (Pfalz 54) airfoil
Max thickness 8.2% at 20% chord
Max camber 4.6% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe326-il) GOE 326 (PFALZ 55) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 326 (PFALZ 55) AIRFOILGottingen 326 (Pfalz 55) airfoil
Max thickness 8.2% at 29.9% chord
Max camber 4.7% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe328-il) GOE 328 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 328 AIRFOILGottingen 328 airfoil
Max thickness 8.2% at 30% chord
Max camber 4.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe329-il) GOE 329 (PFALZ 58) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 329 (PFALZ 58) AIRFOILGottingen 329 (Pfalz 58) airfoil
Max thickness 10.2% at 29.9% chord
Max camber 5.5% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe330-il) GOE 330 (PFALZ 59) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 330 (PFALZ 59) AIRFOILGottingen 330 (Pfalz 59) airfoil
Max thickness 10.2% at 29.9% chord
Max camber 5.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe331-il) GOE 331 (PFALZ 60) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 331 (PFALZ 60) AIRFOILGottingen 331 (Pfalz 60) airfoil
Max thickness 10.6% at 29.9% chord
Max camber 6.9% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe332-il) GOE 332 (PFALZ 61) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 332 (PFALZ 61) AIRFOILGottingen 332 (Pfalz 61) airfoil
Max thickness 11.8% at 29.8% chord
Max camber 6.4% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Page 7 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.