Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
airfoil designation system
|
| gptkbp:basisFor |
further NACA airfoil developments
modern airfoil designations |
| gptkbp:developedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:documentedIn |
gptkb:NACA_Technical_Reports
|
| gptkbp:firstDigitRepresents |
maximum camber
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 5-digit series
|
| gptkbp:introducedIn |
1930s
|
| gptkbp:lastTwoDigitsRepresent |
maximum thickness as percent of chord
|
| gptkbp:notableExample |
gptkb:NACA_23012
gptkb:NACA_24112 |
| gptkbp:notation |
5-digit code
|
| gptkbp:predecessor |
gptkb:NACA_4-digit_series
|
| gptkbp:relatedTo |
gptkb:NACA_airfoil_series
|
| gptkbp:secondDigitRepresents |
position of maximum camber
|
| gptkbp:thirdDigitRepresents |
camber type
|
| gptkbp:usedBy |
aerospace engineers
aircraft designers |
| gptkbp:usedFor |
airfoil design
|
| gptkbp:usedIn |
fixed-wing aircraft
wind tunnel testing |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
| gptkbp:bfsLayer |
6
|