Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:application |
aeronautical engineering
|
| gptkbp:camberPosition |
40% chord
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:developedBy |
gptkb:United_States
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 6509
|
| gptkbp:maximumCamber |
5% of chord
|
| gptkbp:publishedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:series |
gptkb:NACA_6-series
|
| gptkbp:thickness |
9% of chord
|
| gptkbp:usedIn |
aircraft wing design
|
| gptkbp:bfsParent |
gptkb:NACA_6-series_airfoils
|
| gptkbp:bfsLayer |
7
|