Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil_series
|
| gptkbp:application |
gptkb:aircraft
general aviation gliders |
| gptkbp:characteristic |
gentle stall characteristics
improved maximum lift |
| gptkbp:developedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:example |
gptkb:NACA_23012
gptkb:NACA_23015 gptkb:NACA_23018 gptkb:NACA_23021 |
| gptkbp:introducedIn |
1930s
|
| gptkbp:notableFor |
improved lift-to-drag ratio
camber line design variable thickness |
| gptkbp:predecessor |
gptkb:NACA_four-digit_series
|
| gptkbp:usedBy |
various aircraft manufacturers
|
| gptkbp:usedIn |
gptkb:aircraft_wing_design
aeronautical engineering |
| gptkbp:bfsParent |
gptkb:NACA_23012
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 230 series
|