Statements (15)
Predicate | Object |
---|---|
gptkbp:instanceOf |
airfoil
|
gptkbp:application |
aircraft wings
propeller blades |
gptkbp:camber |
0% (symmetric)
|
gptkbp:developedBy |
gptkb:NACA
|
https://www.w3.org/2000/01/rdf-schema#label |
NACA 16-012
|
gptkbp:maximumThicknessLocation |
30% chord from leading edge
|
gptkbp:notableFeature |
laminar flow design
low drag at high speeds |
gptkbp:publishedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
gptkbp:series |
gptkb:NACA_16-series
|
gptkbp:thickness |
12% of chord
|
gptkbp:usedIn |
aeronautical engineering
|
gptkbp:bfsParent |
gptkb:NACA_airfoil_series
|
gptkbp:bfsLayer |
6
|