Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil
|
| gptkbp:application |
aircraft wings
propeller blades |
| gptkbp:camberLineType |
nonlinear
|
| gptkbp:designedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:geometry |
4-digit modified airfoil
|
| gptkbp:maximumCamber |
2% of chord
|
| gptkbp:partOf |
gptkb:NACA_airfoil_series
|
| gptkbp:positionOfMaximumCamber |
30% of chord from leading edge
|
| gptkbp:series |
NACA 23-series
|
| gptkbp:thickness |
12% of chord
|
| gptkbp:usedIn |
aeronautical engineering
|
| gptkbp:bfsParent |
gptkb:NACA_5-digit_airfoils
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
NACA 23112
|