Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Wings
|
| gptkbp:airfoil_family |
Clark airfoils
|
| gptkbp:airfoil_thickness |
12%
|
| gptkbp:application |
gptkb:light_aircraft
gliders sport aircraft |
| gptkbp:characteristic |
high lift
|
| gptkbp:designed_by |
gptkb:David_Clark
|
| https://www.w3.org/2000/01/rdf-schema#label |
Clark Y airfoil
|
| gptkbp:maximum_lift_coefficient |
around 1.5
|
| gptkbp:stall_speed |
gentle stall
|
| gptkbp:type |
cambered airfoil
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:bfsParent |
gptkb:Lockheed_Sirius
gptkb:P-26_A |
| gptkbp:bfsLayer |
5
|