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dc.contributor.advisorNetzer, D.W.
dc.contributor.authorBinn, Brian Andrew
dc.date.accessioned2012-11-16T19:29:20Z
dc.date.available2012-11-16T19:29:20Z
dc.date.issued1979-12
dc.identifier.urihttp://hdl.handle.net/10945/18641
dc.descriptionApproved for public release; distribution unlimiteden_US
dc.description.abstractAn experimental investigation was conducted to determine if there is a relationship between the cold flow characteristics of velocity, pressure distribution, and turbulence intensity and the reacting flow performance and combustion characteristics of a solid fuel ramjet. The effects of configuration cind air flow changes on the above characteristics were examined. Average regression rates and combustion efficiencies were not significantly affected by changes in configuration. These variations in test conditions significantly affected the centerline turbulence intensity but not the near-wall turbulence intensity in cold flow. The use of bypass resulted in decreases in regression rate and efficiencies for all cases. Attainable performance appears to be most strongly related to near-wall turbulence intensity/mixing and to the amount of fuel reaching the aft mixing chamber.en_US
dc.description.urihttp://archive.org/details/comparisonofsoli00binn
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.subject.lcshAeronauticsen_US
dc.titleA comparison of solid fuel ramjet flow characteristics and combustion behavioren_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School
dc.contributor.schoolNaval Postgraduate School
dc.contributor.departmentAeronautics
dc.description.serviceCaptain, United States Air Forceen_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US


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