Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:hasApplication |
control surfaces
horizontal stabilizers vertical stabilizers |
| gptkbp:hasChordLength |
variable
|
| gptkbp:hasLeadingEdgeRadius |
0.015 times chord
|
| gptkbp:hasLiftCurveSlope |
approximately 0.11 per degree
|
| gptkbp:hasMaximumCamber |
0%
|
| gptkbp:hasMaximumThickness |
15% of chord
|
| gptkbp:hasThicknessDistribution |
gptkb:NACA_4-digit_formula
|
| gptkbp:hasTrailingEdge |
sharp
|
| gptkbp:hasZeroLiftAngle |
0 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 0015
|
| gptkbp:partOfSeries |
gptkb:NACA_4-digit_series
|
| gptkbp:symmetry |
true
|
| gptkbp:usedFor |
educational purposes
experimental research |
| gptkbp:usedIn |
aerospace engineering
hydrodynamics wind tunnel testing |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
|
| gptkbp:bfsLayer |
6
|