Statements (14)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:NACA_airfoil_series
|
| gptkbp:application |
aircraft wings
|
| gptkbp:date |
1930s
|
| gptkbp:diameter |
16% of chord
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 23016
|
| gptkbp:length |
1.0
|
| gptkbp:material |
cambered
|
| gptkbp:molt |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:provides_information_on |
lift and drag coefficients
|
| gptkbp:tdp |
2.0%
30% of chord |
| gptkbp:used_in |
aerodynamics research
|