Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:NACA_airfoil_series
|
| gptkbp:application |
aircraft wings
|
| gptkbp:characteristics |
good lift-to-drag ratio
|
| gptkbp:designed_by |
gptkb:NACA
|
| gptkbp:diameter |
15% of chord
|
| gptkbp:first_introduced |
1930s
|
| gptkbp:highest_point |
40% of chord
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 2415
|
| gptkbp:is_tested_for |
gptkb:cave
|
| gptkbp:material |
cambered
|
| gptkbp:related_to |
gptkb:NACA_airfoil_series
|
| gptkbp:tdp |
2.4%
|
| gptkbp:used_in |
aerodynamics research
|