Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil
|
| gptkbp:application |
gptkb:aircraft
general aviation |
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:firstPublished |
1930s
|
| gptkbp:maximumCamber |
2% of chord
|
| gptkbp:maximumCamberPosition |
30% of chord from leading edge
|
| gptkbp:publishedBy |
gptkb:NACA
|
| gptkbp:series |
gptkb:NACA_23000_series
|
| gptkbp:symmetry |
asymmetric
|
| gptkbp:thickness |
10% of chord
|
| gptkbp:usedIn |
aircraft wings
propeller blades |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
NACA 23010
|