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dc.contributor.advisorNetzer, David W.
dc.contributor.authorDuBeau, Robert William
dc.dateJune 1983
dc.date.accessioned2012-11-19T23:58:52Z
dc.date.available2012-11-19T23:58:52Z
dc.date.issued1983-06
dc.identifier.urihttp://hdl.handle.net/10945/19821
dc.description.abstractConstruction, check-out/verification and initial tests of a full scale gas turbine combustor test facility were accomplished. Water cooled gas sampling and stagnation probes and a multiple wavelength light extinction measurement apparatus for determination of mean particulate size were evaluated. The facility will be used for subsequent fuel composition/fuel additive evaluations to determine the resulting effects on soot production and consumption rates.en_US
dc.description.urihttp://archive.org/details/agasturbinecombu1094519821
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.titleA gas turbine combustor test facility for fuel composition investigationsen_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentDepartment of Aeronautics
dc.subject.authorTurboen_US
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.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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