A theory and method of predicting the stability derivatives Clᵦ, Clᵣ, Cn𝗉, and CY𝗉 for wings of arbitrary planform in subsonic flow

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dc.contributor.authorQueijo, M. J.en
dc.contributor.committeememberFletcher, Herman S.en
dc.contributor.committeememberBrown, Clinton E.en
dc.contributor.departmentEngineering Mechanicsen
dc.date.accessioned2014-03-14T21:16:54Zen
dc.date.adate2012-08-01en
dc.date.available2014-03-14T21:16:54Zen
dc.date.issued1963-06-05en
dc.date.rdate2012-08-01en
dc.date.sdate2012-08-01en
dc.description.abstractA theory and method have been developed and design change drawn, for the estimation of certain stability derivatives for wings of arbitrary platform in subsonic flow.en
dc.description.degreePh. D.en
dc.format.extent254 leavesen
dc.format.mediumBTDen
dc.format.mimetypeapplication/pdfen
dc.identifier.otheretd-08012012-040657en
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-08012012-040657/en
dc.identifier.urihttp://hdl.handle.net/10919/39007en
dc.language.isoenen
dc.publisherVirginia Techen
dc.relation.haspartLD5655.V856_1963.Q834.pdfen
dc.relation.isformatofOCLC# 20279114en
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V856 1963.Q834en
dc.subject.lcshAirplanes -- Wings -- Experimentsen
dc.titleA theory and method of predicting the stability derivatives Clᵦ, Clᵣ, Cn𝗉, and CY𝗉 for wings of arbitrary planform in subsonic flowen
dc.typeDissertationen
dc.type.dcmitypeTexten
thesis.degree.disciplineEngineering Mechanicsen
thesis.degree.grantorVirginia Polytechnic Instituteen
thesis.degree.leveldoctoralen
thesis.degree.namePh. D.en

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