Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:airfoilFamily |
gptkb:NACA_4-digit_series
|
| gptkbp:camber |
0%
|
| gptkbp:camberPosition |
0% of chord
|
| gptkbp:designedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 0009
|
| gptkbp:relatedTo |
gptkb:NACA_0012
gptkb:NACA_0015 |
| gptkbp:symmetry |
true
|
| gptkbp:thickness |
gptkb:NACA_4-digit_formula
9% of chord |
| gptkbp:usedIn |
aircraft wing design
aerodynamic research |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
|
| gptkbp:bfsLayer |
6
|