|
gptkbp:instanceOf
|
gptkb:airfoil
|
|
gptkbp:basisFor
|
modern airfoil design
|
|
gptkbp:characteristic
|
mathematically defined shape
|
|
gptkbp:developedBy
|
gptkb:National_Advisory_Committee_for_Aeronautics
|
|
gptkbp:hasApplication
|
fixed-wing aircraft
propeller blades
wind turbine blades
|
|
gptkbp:hasFeature
|
gptkb:NACA_0006
gptkb:NACA_0008
gptkb:NACA_0009
gptkb:NACA_0012
gptkb:NACA_0015
gptkb:NACA_23009
gptkb:NACA_23010
gptkb:NACA_23012
gptkb:NACA_23015
gptkb:NACA_23018
gptkb:NACA_23021
gptkb:NACA_2412
gptkb:NACA_2413
gptkb:NACA_2414
gptkb:NACA_2415
gptkb:NACA_4412
gptkb:NACA_4415
gptkb:NACA_4418
gptkb:NACA_63-215
gptkb:NACA_64-206
gptkb:NACA_65-415
gptkb:NACA_66-415
gptkb:NACA_67-209
|
|
gptkbp:hasType
|
gptkb:NACA_4-digit_series
gptkb:NACA_5-digit_series
gptkb:NACA_6-series
gptkb:NACA_7-series
gptkb:NACA_8-series
|
|
gptkbp:introducedIn
|
1930s
|
|
gptkbp:parameter
|
chord length
maximum camber
maximum thickness
position of maximum camber
|
|
gptkbp:usedIn
|
gptkb:engineer
aeronautical engineering
|
|
gptkbp:bfsParent
|
gptkb:NACA
|
|
gptkbp:bfsLayer
|
6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NACA airfoil
|