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Study of balanced rudders


Metadata FieldValueLanguage
dc.creatorRoche, J. A.
dc.date.accessioned2017-07-24T19:27:10Z
dc.date.available2017-07-24T19:27:10Z
dc.date.created1927-05-21
dc.identifier.urihttp://hdl.handle.net/11200/48919
dc.descriptionThe object of this study was to discover to what extent the rudder can be balanced without causing pilots to complain of an overbalanced condition. The dimensions of the various rudders in use on military airplanes were collected and an expression was developed to show the relative extent to which these rudders are balanced. Pilots observations on the actions of these rudders were also obtained and are given under the heading "Remarks" in the table. This study shows no definite relation between the balanced coefficients and the pilots remarks. It may, therefore, be that rudders which are reported as overbalanced are not really overbalanced, and that other yaw characteristics of the airplane have resulted in producing that impression on the pilot.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 6, no. 586en_US
dc.relation.ispartofseriesMateriel Division report ; Serial no. 2757en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Tail surfacesen_US
dc.subjectSteering-gearen_US
dc.subjectAirplanes--Control surfacesen_US
dc.subjectStability of airplanesen_US
dc.subjectSteering-gearen_US
dc.titleStudy of balanced ruddersen_US
dc.typeTexten_US

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