An investigation of the reacting and non-reacting flow characteristics of solid fuel ramjets

dc.contributor.advisorNetzer, D.W.
dc.contributor.authorScott, Winston Elliott
dc.date.accessioned2012-11-13T23:24:27Z
dc.date.available2012-11-13T23:24:27Z
dc.date.issued1980-09
dc.descriptionDistinguished Alumni Award Program author. CAPT Winston Scott, USN (Ret) (Presented 6 Aug 09)en_US
dc.description.abstractAn investigation was conducted to determine the relation- ship between the non-reacting and the reacting flow characteristics of solid fuel ramjets. Polymethylmethacrylate fuel grains were burned in a ramjet motor on a thrust stand. Combustion efficiency, regression rate profile and pressures were determined for the reacting flows and compared to pro- files obtained in non-reacting flows for velocity, pressure, and near-wall and centerline turbulence intensity. Near-wall turbulence profiles were in agreement with the fuel regression profiles obtained in reacting flows. Combustion efficiency was found to be a strong function of mixture ratio. Near-wall mixing significantly increased fuel regression rate.en_US
dc.description.urihttp://archive.org/details/aninvestigationo1094515779
dc.identifier.oclcocm640235201
dc.identifier.urihttps://hdl.handle.net/10945/15779
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.subject.lcshPhysicsen_US
dc.titleAn investigation of the reacting and non-reacting flow characteristics of solid fuel ramjetsen_US
dc.typeThesisen_US
dspace.entity.typePublication
etd.thesisdegree.disciplinePhysicsen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.nameM.S. in Physicsen_US
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