Statements (17)
Predicate | Object |
---|---|
gptkbp:instanceOf |
airfoil
|
gptkbp:camber |
0%
|
gptkbp:designedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
gptkbp:firstDigitMeaning |
maximum camber (0%)
|
gptkbp:hasNACAcode |
0006
|
https://www.w3.org/2000/01/rdf-schema#label |
NACA 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 |
aerodynamics research
aircraft wing design wind tunnel testing |
gptkbp:bfsParent |
gptkb:NACA_airfoil
|
gptkbp:bfsLayer |
6
|