Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:airfoilFamily |
gptkb:NACA_230_series
|
| gptkbp:camberType |
cambered
|
| gptkbp:designedBy |
gptkb:NACA
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 23012
|
| gptkbp:introducedIn |
1930s
|
| gptkbp:maximumCamber |
2% of chord
|
| gptkbp:maximumCamberPosition |
30% of chord from leading edge
|
| gptkbp:notableFor |
gentle stall characteristics
good lift-to-drag ratio |
| gptkbp:profile |
single-element airfoil
|
| gptkbp:symmetry |
asymmetric
|
| gptkbp:thickness |
12% of chord
|
| gptkbp:usedBy |
gptkb:Mooney_M20
gptkb:Cessna_310 gptkb:Beechcraft_Bonanza gptkb:Navion_aircraft gptkb:Piper_PA-28_Cherokee |
| gptkbp:usedFor |
general aviation aircraft
|
| gptkbp:usedIn |
aerospace engineering
aircraft wings |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
| gptkbp:bfsLayer |
6
|