Airfoil database list (D).
Dormoy to DU 86-137/25 AIRFOIL
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(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 Source UIUC Airfoil Coordinates Database | |
(drgnfly-il) DRAGONFLY CANARD | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Dragonfly Canard airfoil Max thickness 19.3% at 37.6% chord Max camber 6.6% at 40.9% chord Source UIUC Airfoil Coordinates Database | |
(dsma523a-il) DSMA-523A AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | McDonnell/Douglas DSMA-523 transonic airfoil with sharp trailing edge Max thickness 11% at 36% chord Max camber 2.3% at 82% chord Source UIUC Airfoil Coordinates Database | |
(dsma523b-il) DSMA-523B AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | McDonnell/Douglas DSMA-523 transonic airfoil with blunt trailing edge Max thickness 11% at 36% chord Max camber 2.4% at 82% chord Source UIUC Airfoil Coordinates Database | |
(du06-w-200-dt) DU 06-W-200 VAWT airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
 | DU 06-W-200 airfoil for Small Vertical Axis Wind Turbines (VAWT) Max thickness 19.8% at 31.1% chord Max camber 0.5% at 84.6% chord Source TU Delft | |
(du84132v-il) DELFT DU84-132V3 AIRFOIL (MEASURED) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Airfoil measured from an ASW22 wing Max thickness 13.6% at 33.9% chord Max camber 3.1% at 45.3% chord Source UIUC Airfoil Coordinates Database | |
(du8608418-il) DU86-084/18 8.44% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Deflt University DU 86-084/18 low Reynolds number airfoil Max thickness 8.5% at 36.9% chord Max camber 1% at 45.8% chord Source UIUC Airfoil Coordinates Database | |
(du861372-il) DU 86-137/25 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Delft University DU 86-137/25 Airfoil Max thickness 13.6% at 41.6% chord Max camber 0.3% at 1.6% chord Source UIUC Airfoil Coordinates Database | |
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