Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil
|
| gptkbp:analyzes |
computational fluid dynamics
experimental methods |
| gptkbp:appearsIn |
aircraft design
wind tunnel testing |
| gptkbp:basedOn |
camber line
leading edge shape thickness distribution trailing edge shape |
| gptkbp:category |
subsonic airfoils
supersonic airfoils transonic airfoils |
| gptkbp:characterizedBy |
gptkb:NACA_four-digit_series
gptkb:NACA_five-digit_series NACA_six-digit_series |
| gptkbp:designedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:developedBy |
1930s
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA airfoils
|
| gptkbp:influenced |
aircraft performance
aerospace engineering modern airfoil design |
| gptkbp:influencedBy |
airfoil theory
|
| gptkbp:notableEvent |
NACA 0012
NACA 2412 NACA 4412 NACA 23012 NACA 0015 NACA 6409 NACA 0010 NACA 0018 NACA 2415 NACA 4415 |
| gptkbp:relatedTo |
performance metrics
aerodynamic efficiency flow separation control surfaces lift-to-drag ratio stall characteristics boundary layer control airfoil optimization airfoil shape airfoil testing |
| gptkbp:usedFor |
drag reduction
lift generation |
| gptkbp:usedIn |
gptkb:spacecraft
aerodynamics drones helicopters gliders model aircraft full-scale aircraft |