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dc.contributor.authorHedgepeth, John Millsen_US
dc.date.accessioned2014-03-14T21:49:13Z
dc.date.available2014-03-14T21:49:13Z
dc.date.issued1957-03-05en_US
dc.identifier.otheretd-11072012-040239en_US
dc.identifier.urihttp://hdl.handle.net/10919/45527
dc.description.abstract

The panel flutter analysis presented herein has been restricted to the problem of an isolated simply supported plate of uniform thickness. The same type of analysis can be applied, however, to other panel configurations. Clamped panels, integrally stiffened panels, arrays of panels, end others should be amenable to treatment by the model approach based on the static aerodynamic approximation.

en_US
dc.format.mediumBTDen_US
dc.publisherVirginia Techen_US
dc.relation.haspartLD5655.V855_1957.H423.pdfen_US
dc.subjectFlutter (Aerodynamics)en_US
dc.subject.lccLD5655.V855 1957.H423en_US
dc.titleFlutter of rectangular simply supported panels at high supersonic speedsen_US
dc.typeThesisen_US
dc.contributor.departmentApplied Mechanicsen_US
thesis.degree.nameMaster of Scienceen_US
thesis.degree.levelmastersen_US
thesis.degree.grantorVirginia Polytechnic Instituteen_US
dc.contributor.committeechairFrederick, Danielen_US
dc.contributor.committeememberPardue, Louis A.en_US
dc.contributor.committeememberPletta, Dan H.en_US
dc.contributor.committeememberWhittemore, John A.en_US
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-11072012-040239/en_US
dc.date.sdate2012-11-07en_US
dc.date.rdate2012-11-07
dc.date.adate2012-11-07en_US


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