Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil design formula
|
| gptkbp:appliesTo |
subsonic airfoils
|
| gptkbp:basisFor |
gptkb:NACA_6-series_airfoils
|
| gptkbp:developedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:focusesOn |
laminar flow optimization
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 6-series formula
|
| gptkbp:introducedIn |
1940s
|
| gptkbp:notation |
6-digit code
design lift coefficient camber designation position of minimum pressure thickness-to-chord ratio |
| gptkbp:parameter |
chord length
pressure distribution camber maximum thickness location |
| gptkbp:relatedTo |
gptkb:NACA_airfoil_series
|
| gptkbp:usedBy |
aerospace engineers
aircraft designers |
| gptkbp:usedFor |
airfoil shape generation
|
| gptkbp:usedIn |
aeronautical engineering
|
| gptkbp:bfsParent |
gptkb:NACA_63-215
|
| gptkbp:bfsLayer |
7
|