Airfoil database list (W).
WASP (smoothed) to WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL
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(waspsm-il) WASP (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Mike Fox WASP low Reynolds number airfoil Max thickness 9.4% at 27.1% chord Max camber 3% at 37.9% chord Source UIUC Airfoil Coordinates Database | |
(wb13535sm-il) WB-135/35 13.5% smoothed | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Woody Blanchard WB135/35 R/C sailplane airfoil Max thickness 13.6% at 25% chord Max camber 3.8% at 50% chord Source UIUC Airfoil Coordinates Database | |
(wb140-il) WB-140/35/FB 14% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Woody Blanchard WB140/35/FB R/C sailplane airfoil Max thickness 13.9% at 30% chord Max camber 3.7% at 45% chord Source UIUC Airfoil Coordinates Database | |
(whitcomb-il) WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NASA/Langley Whitcomb integral supercritical airfoil Max thickness 11% at 35% chord Max camber 2.4% at 82.5% chord Source UIUC Airfoil Coordinates Database | |
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