Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil
|
| gptkbp:airfoilType |
symmetric
|
| gptkbp:camber |
0%
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:firstPublished |
1933
|
| 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 gptkb:NACA_4-digit_airfoils |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 0012
|