Statements (14)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil
|
| gptkbp:airfoilFamily |
gptkb:NACA_4-digit_series
|
| gptkbp:application |
general aviation
model aircraft |
| gptkbp:camberType |
cambered
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:maximumCamber |
2%
|
| gptkbp:maximumCamberPosition |
40% chord
|
| gptkbp:thickness |
14% chord
|
| gptkbp:usedIn |
aeronautical engineering
aircraft wings |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
NACA 2414
|