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dc.contributor.advisorAkerman, John D.
dc.contributor.authorSollenberger, Robert Lewis
dc.dateJuly 28, 1949
dc.date.accessioned2012-03-14T17:52:47Z
dc.date.available2012-03-14T17:52:47Z
dc.date.issued1949-07-28
dc.identifier.urihttp://hdl.handle.net/10945/6479
dc.descriptionThis thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title.en_US
dc.description.abstractThe primary endeavor in the writer's investigation was to make a preliminary exploration to determine if such a glow could function at all in supersonic airflow, to design apparatus with which an electrical glow discharge from a sharp point could be studied, and also to determine if the glow is pressure or velocity dependent at Mach numbers greater than one,en_US
dc.description.urihttp://www.archive.org/details/investigationsof00soll
dc.language.isoen_US
dc.publisherSt. Paul, Minnesota; University of Minnesotaen_US
dc.subject.lcshAeronauticsen_US
dc.titleInvestigations of an electrical glow discharge, when inserted in supersonic airflow, to determine its dependence on pressure and velocityen_US
dc.typeThesisen_US
dc.contributor.corporateUniversity of Minnesota
dc.contributor.departmentDepartment of Aeronautical Engineering
dc.description.serviceLieutenant Commander, United States Navy .en_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorUniversity of Minnesotaen_US
etd.verifiedyesen_US


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