Statements (14)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:application |
aeronautical engineering
|
| gptkbp:camberType |
asymmetric
|
| gptkbp:designedBy |
gptkb:NACA
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 2415
|
| gptkbp:maximumCamber |
2%
|
| gptkbp:maximumCamberPosition |
40% chord
|
| gptkbp:series |
gptkb:NACA_four-digit_series
|
| gptkbp:thickness |
15% chord
|
| gptkbp:usedIn |
aircraft wings
propeller blades |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
| gptkbp:bfsLayer |
6
|