Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:camberPosition |
40% chord from leading edge
|
| gptkbp:designation |
6-series, 5 tenths minimum pressure at 40% chord, 15% thickness
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:designedFor |
laminar flow
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 65-415
|
| gptkbp:maximumCamber |
4% of chord
|
| gptkbp:publishedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:series |
gptkb:NACA_6-series
|
| gptkbp:thickness |
15% of chord
|
| gptkbp:usedBy |
aerospace engineers
|
| gptkbp:usedIn |
aircraft wing design
|
| gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
| gptkbp:bfsLayer |
6
|