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dc.contributor.advisorMiller, L. Scotten_US
dc.contributor.authorWilliams, Russell Loy
dc.date.accessioned2007-08-23T12:28:54Z
dc.date.available2007-08-23T12:28:54Z
dc.date.issued2005-12
dc.identifier.isbn9780542758034
dc.identifier.othert05045
dc.identifier.otherAAT 1436591:UMI
dc.identifier.urihttp://hdl.handle.net/10057/754
dc.descriptionThesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.en
dc.description"December 2005."en
dc.description.abstractRecent flight test experience and simulator studies have shown that the traditional test for static lateral stability, the steady heading sideslip, in some cases may be overly conservative and place unnecessary restrictions on the aircraft operation or design. In addition, effective dihedral need not be positive in all areas of the flight envelope to provide acceptable handling qualities. Positive static lateral stability is desired so that the aircraft will be safe and that the airplane handling characteristics will be "pleasant." The safety requirement stems from a desire for redundancy in the primary control system. However, safety analysis of modern aircraft often show this redundancy without effective dihedral through other means such as aileron trim, roll spoilers, etc. In terms of handling characteristics, positive static lateral stability usually provides for a more favorable rating of flying qualities by pilots. However, tests have shown that acceptable handling qualities are obtained in most areas of the flight envelope even with negative effective dihedral. Development flight testing on recent business jet aircraft have shown that the aircraft can be operated safely without use of the primary roll control system, even though the basic aircraft did not pass the traditional steady heading sideslip test in all configurations. Furthermore, the handling qualities of the aircraft were considered excellent. (Abstract shortened by UMI.)en
dc.format.extent693686 bytes
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen
dc.rightsCopyright Russell Loy Williams, 2005. All rights reserved.en
dc.subject.lcshElectronic dissertationsen
dc.titleReduced static lateral stability in airplanesen
dc.typeThesisen


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  • AE Theses and Dissertations
    Electronic copies of theses and dissertations defended in the Department of Aerospace Engineering
  • CE Theses and Dissertations
    Doctoral and Master's theses authored by the College of Engineering graduate students
  • Master's Theses
    This collection includes Master's theses completed at the Wichita State University Graduate School (Fall 2005 --)

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