Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:application |
gptkb:trainer_aircraft
general aviation model aircraft |
| gptkbp:camber |
4%
|
| gptkbp:camberPosition |
40% chord
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:firstPublished |
1933
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 4412
|
| gptkbp:maximumLiftCoefficient |
~1.6 (at Re=3 million)
|
| gptkbp:maximumThicknessLocation |
30% chord
|
| gptkbp:notableAircraft |
gptkb:Piper_J-3_Cub
gptkb:Taylorcraft_L-2 gptkb:Aeronca_Champion |
| gptkbp:relatedTo |
gptkb:NACA_0012
gptkb:NACA_2412 |
| gptkbp:series |
gptkb:NACA_4-digit_series
|
| gptkbp:symmetry |
asymmetric
|
| gptkbp:thickness |
12% chord
|
| gptkbp:usedFor |
aerodynamic research
lift generation |
| gptkbp:usedIn |
aerospace engineering
wind tunnel testing aircraft wings propeller blades |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
| gptkbp:bfsLayer |
6
|