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.
(s832-nr) NREL's S832 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
NREL HAWT airfoil S832 Max thickness 14.9% at 44% chord Max camber 5.3% at 44% chord Max Cl/Cd 126 at Re# 500,000 Source NWTC National WInd Technology Center | ||
(e397-il) EPPLER 397 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Eppler E397 human powered aircraft airfoil Max thickness 13.5% at 29.4% chord Max camber 5.3% at 52.1% chord Max Cl/Cd 126 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(nlf1015-il) NASA NLF1015 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
NASA/Langley/Somers-Maughmer NLF(1)-1015 natural laminar flow airfoil Max thickness 15% at 39.8% chord Max camber 4.3% at 62.8% chord Max Cl/Cd 125.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(fx74130wp2-il) 74-130 WP2 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Wortmann 74-130 WP2 airfoil Max thickness 13% at 43.5% chord Max camber 3.9% at 46.7% chord Max Cl/Cd 125.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(mh121-il) MH 121 8.76% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Martin Hepperle MH 121 for tip section of a propeller Max thickness 8.8% at 37.9% chord Max camber 3% at 62.2% chord Max Cl/Cd 125.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(fx72ls160-il) FX 72-LS-160 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Wortmann FX 72-LS-160 airfoil Max thickness 16% at 37.1% chord Max camber 8.2% at 43.5% chord Max Cl/Cd 125.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(fx63120-il) FX 63-120 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Wortmann FX 63-120 airfoil Max thickness 12% at 30.8% chord Max camber 5.2% at 50% chord Max Cl/Cd 125.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(mh116-il) MH 116 9.84% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Martin Hepperle MH 116 for a propeller for ultralight Max thickness 9.9% at 32.4% chord Max camber 4.1% at 46.4% chord Max Cl/Cd 125.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(fx63137sm-il) FX 63-137 13.7% smoothed | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Wortmann FX 63-137 airfoil (smoothed) Max thickness 13.7% at 30.9% chord Max camber 5.8% at 56.5% chord Max Cl/Cd 125.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(fx62k131-il) WORTMANN FX 62-K-131 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Wortmann FX 62-K-131/17 airfoil Max thickness 13.1% at 40.2% chord Max camber 3.9% at 53.3% chord Max Cl/Cd 125.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database |
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