Airfoil database search
Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.
(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 | |
Gottingen 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 | |
Gottingen 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 | |
Gottingen 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 | |
Gottingen 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 | |
Gottingen 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 | |
Gottingen 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 | |
Gottingen 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 | |
Gottingen 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 | |
Gottingen 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 | |
Gottingen 325 (Pfalz 54) airfoil Max thickness 8.2% at 20% chord Max camber 4.6% at 30% chord Source UIUC Airfoil Coordinates Database |
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