Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:camberPosition |
40% chord
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:designedFor |
laminar flow
|
| gptkbp:firstPublished |
1940s
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 66-415
|
| 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:usedIn |
gptkb:Mooney_M20
gptkb:Piper_PA-28_Cherokee aeronautical engineering aircraft wing design |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
|
| gptkbp:bfsLayer |
6
|