|
gptkbp:instanceOf
|
gptkb:Aircraft_control_surface
|
|
gptkbp:canBe
|
Split
All-moving
Anti-servo tab
Electrically actuated
Hydraulically actuated
Manually actuated
Servo tab
Trimmable
|
|
gptkbp:controls
|
gptkb:Pitch
|
|
gptkbp:criticalFor
|
gptkb:Landing
gptkb:Takeoff
Maneuvering
|
|
gptkbp:effectOfDownMovement
|
Nose up
|
|
gptkbp:effectOfUpMovement
|
Nose down
|
|
gptkbp:failureMode
|
Loss of pitch control
|
|
gptkbp:foundIn
|
T-tail
V-tail
Canard configuration
Conventional tail
|
|
gptkbp:influenced
|
gptkb:Lift
Aircraft stability
Angle of attack
|
|
gptkbp:introducedIn
|
Early 20th century
|
|
gptkbp:location
|
Horizontal stabilizer
|
|
gptkbp:material
|
gptkb:wood
Aluminum
Composite materials
|
|
gptkbp:movement
|
gptkb:Up
gptkb:Down
|
|
gptkbp:operatedBy
|
gptkb:Pilot
Control column
|
|
gptkbp:partOf
|
gptkb:Empennage
|
|
gptkbp:regulates
|
gptkb:Descent
Climb
Level flight
|
|
gptkbp:relatedTo
|
gptkb:Aileron
gptkb:Rudder
Stabilator
|
|
gptkbp:requires
|
Hinges
Aircraft pitch control
Control linkage
Trim tab
|
|
gptkbp:subjectOf
|
Aerodynamics research
Flight control system studies
|
|
gptkbp:usedOn
|
gptkb:aircraft
|
|
gptkbp:bfsParent
|
gptkb:Rudder
|
|
gptkbp:bfsLayer
|
8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Elevator (aeronautics)
|