Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:application |
general aviation
aerodynamic research |
| gptkbp:camberType |
cambered
|
| gptkbp:designedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 4415
|
| gptkbp:introducedIn |
1930s
|
| gptkbp:maximumCamber |
4%
|
| gptkbp:maximumCamberPosition |
40% chord
|
| gptkbp:series |
gptkb:NACA_four-digit_airfoil_series
|
| gptkbp:symmetry |
false
|
| gptkbp:thickness |
15% chord
|
| gptkbp:thicknessType |
moderate
|
| gptkbp:usedIn |
model aircraft
aircraft wings wind turbine blades |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
|
| gptkbp:bfsLayer |
6
|