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dc.contributor.authorHaile, James Ernesten
dc.date.accessioned2016-02-01T14:44:56Zen
dc.date.available2016-02-01T14:44:56Zen
dc.date.issued1968en
dc.identifier.urihttp://hdl.handle.net/10919/64581en
dc.description.abstractA theoretical analysis of the static and dynamic characteristics of an entry vehicle utilizing the decoupled landing concept has been conducted. A hypersonic arbitrary-body aerodynamic computer program was used to determine the aerodynamics of the basic body. Three theories were used and compared with data obtained for a Mach number equal to nineteen. Several stabilizing devices were investigated to determine which were the most effective in providing static stability. To evaluate the lateral-directional handling qualities, a ωΘd coupling parameter along with the parameter abs(Θ/β) were derived to be applicable during hypersonic entry. Equations were also derived for determining the contribution of the stabilizing devices to the dynamic stability derivatives. In the evaluation of the vehicle dynamic characteristics linearized equations of motion for the longitudinal and lateral directional modes were used at several points along a maximum performance trajectory. The parameters considered throughout the trajectory were the period and the time to damp to one-half amplitude.en
dc.format.extent44 leavesen
dc.format.mimetypeapplication/pdfen
dc.language.isoen_USen
dc.publisherVirginia Polytechnic Instituteen
dc.relation.isformatofOCLC# 20147592en
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V855 1968.H32en
dc.subject.lcshLanding aids (Aeronautics)en
dc.titleAn analysis of the static and dynamic characteristics of a decoupled landing entry vehicleen
dc.typeThesisen
dc.contributor.departmentAerospace Engineeringen
dc.description.degreeMaster of Scienceen
thesis.degree.nameMaster of Scienceen
thesis.degree.levelmastersen
thesis.degree.grantorVirginia Polytechnic Instituteen
thesis.degree.disciplineAerospace Engineeringen
dc.type.dcmitypeTexten


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