Statements (15)
Predicate | Object |
---|---|
gptkbp:instanceOf |
airfoil
|
gptkbp:airfoilFamily |
gptkb:NACA_6-series
|
gptkbp:camberPosition |
40% chord from leading edge
|
gptkbp:designedBy |
gptkb:NACA
|
https://www.w3.org/2000/01/rdf-schema#label |
NACA 6609
|
gptkbp:introducedIn |
1940s
|
gptkbp:maximumCamber |
6% of chord
|
gptkbp:optimizedFor |
laminar flow
|
gptkbp:thickness |
9% of chord
|
gptkbp:usedBy |
model aircraft
general aviation aircraft |
gptkbp:usedFor |
aircraft wings
|
gptkbp:usedIn |
aeronautical engineering
|
gptkbp:bfsParent |
gptkb:NACA_6-series_airfoils
|
gptkbp:bfsLayer |
7
|