Publication:
Projectile thrust-drag optimization with external burning

dc.contributor.advisorFuhs, Allen E.
dc.contributor.authorSmithey, William John Henry
dc.contributor.departmentAeronautics
dc.contributor.schoolNaval Postgraduate School
dc.date.accessioned2012-11-14T00:00:23Z
dc.date.available2012-11-14T00:00:23Z
dc.date.issued1974-06
dc.description.abstractExternal burning increases base pressure. The characteristic and linearized equations with heat addition are discuss ed, and the condition for maintaining irrotationa ity with heat addition is derived. A transition model, which extends the Crocco-Lees base flow model, and a spin model are discussed. Computed results are compared with experiment. The optimum location for supersonic external burning is given.en_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.
dc.description.serviceCommander, United States Navyen_US
dc.description.urihttp://archive.org/details/projectilethrust1094517185
dc.identifier.urihttps://hdl.handle.net/10945/17185
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.subject.lcshAeronauticsen_US
dc.titleProjectile thrust-drag optimization with external burningen_US
dc.typeThesisen_US
dspace.entity.typePublication
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
etd.thesisdegree.levelDoctoralen_US
etd.thesisdegree.namePh.D.en_US
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