Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil
|
| gptkbp:camber |
0%
|
| gptkbp:designedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:firstDigitMeaning |
maximum camber (0%)
|
| gptkbp:hasNACAcode |
0006
|
| gptkbp:lastTwoDigitsMeaning |
maximum thickness (6% of chord)
|
| gptkbp:partOf |
gptkb:NACA_four-digit_series
|
| gptkbp:secondDigitMeaning |
position of maximum camber (0%)
|
| gptkbp:symmetry |
symmetric
|
| gptkbp:thickness |
gptkb:NACA_4-digit_formula
6% of chord |
| gptkbp:usedIn |
gptkb:aircraft_wing_design
aerodynamics research wind tunnel testing |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 0006
|