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.
(cp-180-050-gn) Cambered plate C=18% T=5% R=0.78 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file | |
 | HAWT pipe blade with coordinates based on top surface. Camber=18% Wall thickness=5% Radius=0.784 Max thickness 5% at 3.2% chord Max camber 16.4% at 49.3% chord Max Cl/Cd 29.8 at Re# 1,000,000 Source Generated | |
(hs1430-il) HAM-STD HS1-430 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | HS1 family of prop airfoils from US Patent No. 4 Max thickness 30% at 34% chord Max camber 3% at 44% chord Max Cl/Cd 29.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(hs1430-il) HAM-STD HS1-430 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
| HS1 family of prop airfoils from US Patent No. 4 Max thickness 30% at 34% chord Max camber 3% at 44% chord Max Cl/Cd 29.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(ah93w480b-il) AH 93-W-480B | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Althaus AH 93-W-480B airfoil for use on wind turbines (W) Max thickness 47.8% at 44.1% chord Max camber 3.6% at 44.1% chord Max Cl/Cd 28 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(ah93w480b-il) AH 93-W-480B | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
| Althaus AH 93-W-480B airfoil for use on wind turbines (W) Max thickness 47.8% at 44.1% chord Max camber 3.6% at 44.1% chord Max Cl/Cd 26.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(ys900-il) YS-900 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | YS900 hyrdofoil (Shen / Eppler) Max thickness 9% at 52.5% chord Max camber 0% at 0% chord Max Cl/Cd 22.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe570-il) GOE 570 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 570 airfoil Max thickness 33.7% at 30% chord Max camber 9.7% at 40% chord Max Cl/Cd 20.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(griffith30symsuction-il) Griffith 30% Suction Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Griffith 30% suction airfoil Max thickness 30.6% at 49.3% chord Max camber 0% at 0% chord Max Cl/Cd 17.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe570-il) GOE 570 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
| Gottingen 570 airfoil Max thickness 33.7% at 30% chord Max camber 9.7% at 40% chord Max Cl/Cd 16.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(griffith30symsuction-il) Griffith 30% Suction Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
| Griffith 30% suction airfoil Max thickness 30.6% at 49.3% chord Max camber 0% at 0% chord Max Cl/Cd 15.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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