Statements (13)
Predicate | Object |
---|---|
gptkbp:instanceOf |
airfoil
|
gptkbp:airfoilType |
cambered
|
gptkbp:designedBy |
gptkb:NACA
|
https://www.w3.org/2000/01/rdf-schema#label |
NACA 23024
|
gptkbp:maximumCamber |
2% of chord
|
gptkbp:maximumCamberPosition |
30% of chord from leading edge
|
gptkbp:publishedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
gptkbp:series |
gptkb:NACA_23000_series
|
gptkbp:thickness |
24% of chord
|
gptkbp:usedFor |
wing design
|
gptkbp:usedIn |
aeronautical engineering
|
gptkbp:bfsParent |
gptkb:NACA_airfoil_series
|
gptkbp:bfsLayer |
6
|