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- Rudder_ratio abstract "Rudder ratio refers to a value that is monitored by the computerized flight control systems in modern aircraft. The ratio relates the aircraft airspeed to the rudder deflection setting that's in effect at the time. As an aircraft accelerates the deflection of the rudder needs to be reduced proportionately within the range of the rudder pedal depression by the pilot. This automatic reduction process is needed because if the rudder is fully deflected when the aircraft is in high speed flight, it will cause the plane to sharply and violently yaw, or swing from side to side, leading to loss of control and rudder, tail and other damages, even causing the aircraft to crash.".
- Rudder_ratio wikiPageID "2220565".
- Rudder_ratio wikiPageRevisionID "544060309".
- Rudder_ratio hasPhotoCollection Rudder_ratio.
- Rudder_ratio subject Category:Aerospace_engineering.
- Rudder_ratio subject Category:Engineering_ratios.
- Rudder_ratio type Abstraction100002137.
- Rudder_ratio type EngineeringRatios.
- Rudder_ratio type MagnitudeRelation113815152.
- Rudder_ratio type Ratio113819207.
- Rudder_ratio type Relation100031921.
- Rudder_ratio comment "Rudder ratio refers to a value that is monitored by the computerized flight control systems in modern aircraft. The ratio relates the aircraft airspeed to the rudder deflection setting that's in effect at the time. As an aircraft accelerates the deflection of the rudder needs to be reduced proportionately within the range of the rudder pedal depression by the pilot.".
- Rudder_ratio label "Rudder ratio".
- Rudder_ratio label "Rudder ratio".
- Rudder_ratio sameAs Rudder_ratio.
- Rudder_ratio sameAs m.06wzky.
- Rudder_ratio sameAs Q3942228.
- Rudder_ratio sameAs Q3942228.
- Rudder_ratio sameAs Rudder_ratio.
- Rudder_ratio wasDerivedFrom Rudder_ratio?oldid=544060309.
- Rudder_ratio isPrimaryTopicOf Rudder_ratio.