Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:camberPosition |
40% chord
|
| gptkbp:camberType |
single camber
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designedBy |
gptkb:NACA
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 24112
|
| gptkbp:maximumCamber |
2%
|
| gptkbp:publishedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:series |
NACA 4-digit airfoil series
|
| gptkbp:thickness |
gptkb:NACA_4-digit_formula
12% chord |
| gptkbp:usedIn |
aerospace engineering
aircraft wing design |
| gptkbp:bfsParent |
gptkb:NACA_5-digit_series
|
| gptkbp:bfsLayer |
7
|