Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil series
|
| gptkbp:designedFor |
transonic flight
|
| gptkbp:developedBy |
gptkb:NASA
|
| gptkbp:feature |
improved lift-to-drag ratio
aft-loaded pressure distribution high drag-divergence Mach number relatively flat upper surface supercritical upper surface |
| https://www.w3.org/2000/01/rdf-schema#label |
NASA SC(2) airfoil series
|
| gptkbp:introducedIn |
1970s
|
| gptkbp:namingConvention |
SC(2)-XXX(Y)
|
| gptkbp:predecessor |
gptkb:NACA_airfoil_series
|
| gptkbp:relatedTo |
gptkb:supercritical_airfoil
|
| gptkbp:usedFor |
supercritical wing design
|
| gptkbp:usedIn |
gptkb:aircraft
aeronautical engineering |
| gptkbp:bfsParent |
gptkb:NASA_airfoil_series
|
| gptkbp:bfsLayer |
7
|