Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil
|
| gptkbp:designedBy |
gptkb:NACA
|
| gptkbp:firstDigitMeaning |
gptkb:6-series_(laminar_flow)
|
| 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 |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 64-206
|