Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil_designation_system
|
| gptkbp:developedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:focusesOn |
laminar flow airfoils
|
| gptkbp:introducedIn |
1940s
|
| gptkbp:notableExample |
gptkb:NACA_6412
gptkb:NACA_6509 NACA 6615 |
| gptkbp:notation |
design lift coefficient
series number location of minimum pressure modification letter thickness-to-chord ratio |
| gptkbp:predecessor |
gptkb:NACA_4-digit_series
gptkb:NACA_5-digit_series |
| gptkbp:relatedTo |
gptkb:NACA_airfoil
aerodynamics airfoil design |
| gptkbp:usedBy |
aircraft designers
|
| gptkbp:usedFor |
airfoil classification
|
| gptkbp:usedIn |
aeronautical engineering
|
| gptkbp:bfsParent |
gptkb:NACA_6-series_airfoils
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 6-series code
|