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.
(m10-il) NACA M10 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA/Munk M-10 airfoil Max thickness 6.2% at 30% chord Max camber 1.9% at 30% chord Max Cl/Cd 75.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(npl9660-il) NPL 9660 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NPL 9660 rotorcraft airfoil Max thickness 11.3% at 34.2% chord Max camber 1% at 19.8% chord Max Cl/Cd 75.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fxl142k-il) FX LIII-142 K 25 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX LIII-142 K 25 airfoil Max thickness 14.2% at 30.9% chord Max camber 0% at 0% chord Max Cl/Cd 75.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(giiid-il) GIII BL86 AIRFOIL (modified line 31) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Grumman/Gulfstream GIII transonic airfoils Max thickness 9.7% at 39.8% chord Max camber 1% at 29.8% chord Max Cl/Cd 75.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(dormoy-il) Dormoy | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Dormoy airfoil Max thickness 9% at 30% chord Max camber 2.9% at 40% chord Max Cl/Cd 75.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(giiic-il) GIII BL75 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Grumman/Gulfstream GIII transonic airfoils Max thickness 9.9% at 39.8% chord Max camber 0.9% at 29.8% chord Max Cl/Cd 75.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s9026-il) S9026 (9.5%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S9026 (9.5%) symmetrical horizontal stab airfoil used on the Opus R/C sailplane Max thickness 9.5% at 27.3% chord Max camber 0% at 0% chord Max Cl/Cd 75.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx76100-il) WORTMANN FX 76-100 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 76-100 symmetrical airfoil Max thickness 10.1% at 27.9% chord Max camber 0% at 0% chord Max Cl/Cd 75.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(p51htip-il) NACA 66 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 66 Max thickness 12% at 45% chord Max camber 1.3% at 47.5% chord Max Cl/Cd 75.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(naca0015-il) NACA 0015 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 0015 airfoil Max thickness 15% at 30% chord Max camber 0% at 0% chord Max Cl/Cd 75.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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