Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:NACA_airfoil_series
|
| gptkbp:application |
aircraft wings
|
| gptkbp:first_introduced |
1930s
|
| gptkbp:floors |
0.4
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 23018
|
| gptkbp:material |
cambered
|
| gptkbp:max_takeoff_weight |
10% of chord
|
| gptkbp:molt |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:speed |
12 degrees
|
| gptkbp:tdp |
2.3%
30% of chord |