Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil series
|
| gptkbp:characteristic |
improved lift-to-drag ratio
maximum camber at 15% chord |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:NACA
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 23000
|
| gptkbp:introducedIn |
1930s
|
| gptkbp:relatedTo |
gptkb:NACA_airfoil
|
| gptkbp:series |
gptkb:NACA_23000_series
|
| gptkbp:usedFor |
aircraft wings
|
| gptkbp:usedIn |
aeronautical engineering
|
| gptkbp:bfsParent |
gptkb:NACA_23021
|
| gptkbp:bfsLayer |
7
|