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.
(goe379-il) GOE 379 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 379 airfoil Max thickness 6.5% at 30% chord Max camber 5.2% at 40% chord Max Cl/Cd 77.7 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe287-il) GOE 287 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 287 airfoil Max thickness 8.9% at 29.9% chord Max camber 4.9% at 39.9% chord Max Cl/Cd 77.7 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(spicasm-il) SPICA 11.73% smoothed | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Anderson SPICA R/C sailplane airfoil (smoothed) Max thickness 11.7% at 30% chord Max camber 4.7% at 35% chord Max Cl/Cd 77.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(k3311sm-il) K3311 (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Leon Kincaid K3311 airfoil (smoothed) Max thickness 11% at 30.6% chord Max camber 3.2% at 41.6% chord Max Cl/Cd 77.6 at Re# 200,000 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 | |
 | Gottingen 115 (MVA MK.2) airfoil Max thickness 9.7% at 29.7% chord Max camber 3.7% at 39.7% chord Max Cl/Cd 77.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe528-il) GOE 528 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 528 airfoil Max thickness 12.5% at 29.8% chord Max camber 6.2% at 39.8% chord Max Cl/Cd 77.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(e197-il) E197 (13.49%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E197 low Reynolds number airfoil Max thickness 13.5% at 34.6% chord Max camber 2.8% at 43.7% chord Max Cl/Cd 77.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe596-il) GOE 596 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 596 airfoil Max thickness 9.8% at 30% chord Max camber 4% at 40% chord Max Cl/Cd 77.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe392-il) GOE 392 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 392 airfoil Max thickness 10.2% at 30% chord Max camber 4.8% at 40% chord Max Cl/Cd 77.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe361-il) GOE 361 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 361 airfoil Max thickness 6.8% at 20% chord Max camber 5.5% at 40% chord Max Cl/Cd 77.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
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