Statements (19)
Predicate | Object |
---|---|
gptkbp:instanceOf |
airfoil
|
gptkbp:application |
general aviation
model aircraft |
gptkbp:camberType |
cambered
|
gptkbp:countryOfOrigin |
gptkb:United_States
|
gptkbp:designedBy |
gptkb:NACA
|
gptkbp:firstPublished |
1940s
|
https://www.w3.org/2000/01/rdf-schema#label |
NACA 6412
|
gptkbp:maximumCamber |
4% of chord
|
gptkbp:maximumCamberPosition |
40% of chord from leading edge
|
gptkbp:series |
gptkb:NACA_6-series
|
gptkbp:symmetry |
asymmetric
|
gptkbp:thickness |
gptkb:NACA_6-series_formula
12% of chord |
gptkbp:usedFor |
propeller blades
wing design |
gptkbp:usedIn |
aeronautical engineering
|
gptkbp:bfsParent |
gptkb:NACA_6-series_airfoils
|
gptkbp:bfsLayer |
7
|