Statements (16)
Predicate | Object |
---|---|
gptkbp:instanceOf |
airfoil
|
gptkbp:camberPosition |
40% chord from leading edge
|
gptkbp:camberType |
single camber
|
gptkbp:designedBy |
gptkb:NACA
|
gptkbp:designedFor |
laminar flow
|
https://www.w3.org/2000/01/rdf-schema#label |
NACA 63-215
|
gptkbp:maximumCamber |
2% of chord
|
gptkbp:series |
gptkb:NACA_6-series
|
gptkbp:symmetry |
asymmetric
|
gptkbp:thickness |
gptkb:NACA_6-series_formula
15% of chord |
gptkbp:usedIn |
aeronautical engineering
aircraft wing design |
gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
gptkbp:bfsLayer |
6
|