Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil_series
|
| gptkbp:basisFor |
airfoil selection in WWII aircraft
|
| gptkbp:developedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:introduced |
1940s
|
| gptkbp:namingConvention |
7-XX-XX
|
| gptkbp:notableFor |
improved drag characteristics
laminar flow design |
| gptkbp:optimizedFor |
specific lift coefficient
|
| gptkbp:predecessor |
gptkb:NACA_4-series
gptkb:NACA_5-series |
| gptkbp:relatedTo |
gptkb:NACA_airfoil_series
|
| gptkbp:successor |
gptkb:NACA_8-series
|
| gptkbp:usedBy |
aerospace engineers
|
| gptkbp:usedIn |
gptkb:aircraft_wing_design
aeronautics aerospace engineering propeller design |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 7-series
|