Statements (14)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:NACA_airfoil_series
gptkb:Supermarine_S.6 |
| gptkbp:application |
aircraft wings
|
| gptkbp:diameter |
12% of chord
|
| gptkbp:floors |
0.5
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 23012
|
| gptkbp:length |
1.0
|
| gptkbp:material |
cambered
|
| gptkbp:series |
gptkb:NACA_2300_series
|
| gptkbp:speed |
12 degrees
|
| gptkbp:tdp |
2.0%
30% of chord |