Statements (22)
Predicate | Object |
---|---|
gptkbp:instanceOf |
airfoil
|
gptkbp:airfoilType |
symmetric
|
gptkbp:camber |
0%
|
gptkbp:designedBy |
gptkb:NACA
|
gptkbp:firstPublished |
1933
|
https://www.w3.org/2000/01/rdf-schema#label |
NACA 0012
|
gptkbp:leadingEdgeRadius |
2.87% of chord
|
gptkbp:maximumLiftCoefficient |
~1.6 (at Re=9 million)
|
gptkbp:NACAseries |
gptkb:NACA_4-digit_series
|
gptkbp:thickness |
gptkb:NACA_4-digit_formula
12% of chord |
gptkbp:usedFor |
educational purposes
benchmarking computational fluid dynamics experimental validation |
gptkbp:usedIn |
aerodynamic research
wind tunnel testing aircraft wings propeller blades |
gptkbp:zeroLiftAngle |
0 degrees
|
gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
gptkbp:bfsLayer |
6
|