Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:camberType |
asymmetric
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:hasSymmetricalCounterpart |
gptkb:NACA_0012
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 2412
|
| gptkbp:introducedIn |
1930s
|
| gptkbp:maximumCamber |
2%
|
| gptkbp:maximumCamberPosition |
40% chord
|
| gptkbp:series |
gptkb:NACA_four-digit_airfoil_series
|
| gptkbp:thickness |
12% chord
|
| gptkbp:usedBy |
gptkb:Piper_Cherokee
gptkb:Aeronca_Champion Cessna 172 |
| gptkbp:usedFor |
general aviation aircraft
|
| gptkbp:usedIn |
aeronautical engineering
aircraft wings |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
| gptkbp:bfsLayer |
6
|