Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:airfoilFamily |
gptkb:NACA_6-series
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:designedFor |
laminar flow
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 67-209
|
| gptkbp:introducedIn |
1940s
|
| gptkbp:maximumCamber |
2% of chord
|
| gptkbp:thickness |
9% of chord
|
| gptkbp:usedBy |
aerospace industry
|
| gptkbp:usedFor |
aircraft wings
|
| gptkbp:usedIn |
aeronautical engineering
|
| gptkbp:bfsParent |
gptkb:NACA_airfoil
|
| gptkbp:bfsLayer |
6
|