Show simple item record

dc.contributor.authorHalter, Megaera C.en
dc.date.accessioned2014-03-14T21:40:33Zen
dc.date.available2014-03-14T21:40:33Zen
dc.date.issued1988-05-15en
dc.identifier.otheretd-07152010-020313en
dc.identifier.urihttp://hdl.handle.net/10919/43753en
dc.description.abstractA reduced order model describing the energy and heading angle dynamics of a scramjet missile is developed using a singular perturbation technique. The cruise analysis is briefly reviewed to determine the conditions at which the missile will cruise most efficiently. The turn and climb performance of the missile over the conditions of interest is then examined and a family of extremal trajectories is constructed which asymptotically approach the cruise at an intermediate altitude.en
dc.format.extentxiii, 96 leavesen
dc.format.mediumBTDen
dc.format.mimetypeapplication/pdfen
dc.publisherVirginia Techen
dc.relation.isformatofOCLC# 18959333en
dc.relation.haspartLD5655.V855_1988.H345.pdfen
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V855 1988.H345en
dc.subject.lcshGuided missiles -- Control systemsen
dc.titleEnergy-turns analysis for a scramjet powered missleen
dc.typeThesisen
dc.contributor.departmentAerospace Engineeringen
dc.description.degreeMaster of Scienceen
thesis.degree.nameMaster of Scienceen
thesis.degree.levelmastersen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.disciplineAerospace Engineeringen
dc.contributor.committeechairCliff, Eugene M.en
dc.contributor.committeememberLutze, Frederick H. Jr.en
dc.contributor.committeememberMarchman, James F. IIIen
dc.type.dcmitypeTexten
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-07152010-020313/en
dc.date.sdate2010-07-15en
dc.date.rdate2010-07-15en
dc.date.adate2010-07-15en


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record