Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil series
|
| gptkbp:characteristic |
maximum lift-to-drag ratio at a specified lift coefficient
|
| gptkbp:developedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:feature |
laminar flow design
8-series airfoil |
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 8-XXX
|
| gptkbp:introducedIn |
1940s
|
| gptkbp:namingConvention |
8-XXX indicates 8-series, with XXX specifying design parameters
|
| gptkbp:relatedTo |
gptkb:NACA_airfoil_series
|
| gptkbp:usedFor |
aircraft wing design
|
| gptkbp:usedIn |
aeronautical engineering
|
| gptkbp:bfsParent |
gptkb:NACA_8-series
|
| gptkbp:bfsLayer |
7
|