Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil family
|
| gptkbp:application |
propeller blades
wind turbine blades |
| gptkbp:basisFor |
gptkb:NACA_6-series_airfoils
|
| gptkbp:camberLine |
designed for specific lift coefficient
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:documentedIn |
NACA Technical Report 824
|
| gptkbp:example |
gptkb:NACA_23012
gptkb:NACA_23112 gptkb:NACA_24112 |
| gptkbp:feature |
improved lift characteristics
better control of maximum lift customizable design parameters modified camber line |
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 5-series airfoils
|
| gptkbp:introducedIn |
1930s
|
| gptkbp:namingConvention |
5-digit code
|
| gptkbp:predecessor |
gptkb:NACA_4-series_airfoils
|
| gptkbp:usedFor |
aircraft wing design
|
| gptkbp:usedIn |
aeronautical engineering
|
| gptkbp:bfsParent |
gptkb:NACA_6-series_airfoils
|
| gptkbp:bfsLayer |
7
|