NACA 0012

GPTKB entity

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