Statements (17)
Predicate | Object |
---|---|
gptkbp:instanceOf |
airfoil
|
gptkbp:designedBy |
gptkb:NACA
|
gptkbp:firstDigitMeaning |
gptkb:6-series_(laminar_flow)
|
https://www.w3.org/2000/01/rdf-schema#label |
NACA 64-206
|
gptkbp:intendedUse |
gptkb:aircraft
|
gptkbp:laminarFlowDesign |
yes
|
gptkbp:lastTwoDigitsMeaning |
maximum thickness of 6% chord
|
gptkbp:maximumCamber |
2% of chord
|
gptkbp:secondDigitMeaning |
location of minimum pressure at 40% chord
|
gptkbp:series |
gptkb:NACA_6-series
|
gptkbp:thickness |
6% of chord
|
gptkbp:thirdDigitMeaning |
design lift coefficient of 0.2
|
gptkbp:usedIn |
gptkb:engineer
aeronautical research |
gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
gptkbp:bfsLayer |
6
|