Statements (12)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil series
|
| gptkbp:appliesTo |
aircraft wings
|
| gptkbp:developedBy |
gptkb:NACA
|
| gptkbp:feature |
reduced drag
delayed transition to turbulent flow |
| https://www.w3.org/2000/01/rdf-schema#label |
6-series (laminar flow)
|
| gptkbp:introducedIn |
1940s
|
| gptkbp:partOf |
gptkb:NACA_airfoil_series
|
| gptkbp:purpose |
maximize laminar flow
|
| gptkbp:usedIn |
aeronautical engineering
|
| gptkbp:bfsParent |
gptkb:NACA_64-206
|
| gptkbp:bfsLayer |
7
|