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The application of intermittent detonative combustion to jet propulsion

dc.contributor.advisorTaylor, E. B.
dc.contributor.advisorHawthorne, W. R.
dc.contributor.authorUtgoff, Vadym Victorovich
dc.date1949
dc.date.accessioned2012-03-14T17:52:01Z
dc.date.available2012-03-14T17:52:01Z
dc.date.issued1949
dc.identifier.urihttp://hdl.handle.net/10945/6329
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.abstractIt is the purpose of this paper to describer a thermal jet based on intermittent detonative combustion already developed; to attempt an analysis of the process involved; and to report the results of experiments conducted by the author in connection herewith.en_US
dc.description.urihttp://archive.org/details/thepplicationofi109456329
dc.language.isoen_US
dc.publisherCambridge, Massachusetts; Massachusetts Institute of Technologyen_US
dc.subject.lcshAeronauticsen_US
dc.titleThe application of intermittent detonative combustion to jet propulsionen_US
dc.typeThesisen_US
dc.contributor.corporateMassachusetts Institute of Technology
dc.contributor.departmentAeronautical Engineering
dc.description.serviceLieutenant Commander, United States Navyen_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorMassachusetts Institute of Technologyen_US
etd.verifiedyesen_US


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