An investigation of the variation of elevator power and damping in pitch with Mach number for an FJ-3B Fury Jet airplane through steady state flight tests

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dc.contributor.authorFoxgrover, James H.
dc.contributor.authorMandeville, Robert C.
dc.contributor.departmentDept. of Aeronautical Engineering
dc.date.accessioned2012-10-10T19:59:51Z
dc.date.available2012-10-10T19:59:51Z
dc.date.issued1959
dc.description.serviceU.S. Navy (U.S.N.) authors.en_US
dc.description.urihttp://archive.org/details/aninvestigationo1094514364
dc.identifier.oclcocn640242626
dc.identifier.urihttps://hdl.handle.net/10945/14364
dc.language.isoen_US
dc.publisherPrinceton Universityen_US
dc.subject.lcshAeronauticsen_US
dc.titleAn investigation of the variation of elevator power and damping in pitch with Mach number for an FJ-3B Fury Jet airplane through steady state flight testsen_US
dc.typeThesisen_US
dspace.entity.typePublication
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorPrinceton Universityen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.nameM.S. in Engineeringen_US
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