Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:NACA_airfoil_series
|
| gptkbp:application |
aircraft wings
|
| gptkbp:design |
lift generation
|
| gptkbp:developed_by |
gptkb:NACA
|
| gptkbp:fins |
gptkb:NACA_four-digit_series
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 0010
|
| gptkbp:length |
variable
|
| gptkbp:max_takeoff_weight |
10% of chord
|
| gptkbp:orbital_inclination |
varies for performance analysis
|
| gptkbp:type |
symmetrical airfoil
|
| gptkbp:used_in |
aerodynamic testing
|