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dc.contributor.advisorLayton, Donald M.
dc.contributor.authorLeins, William M.
dc.dateMarch 1975
dc.date.accessioned2012-11-20T00:27:14Z
dc.date.available2012-11-20T00:27:14Z
dc.date.issued1975-03
dc.identifier.urihttp://hdl.handle.net/10945/21122
dc.descriptionApproved for public release; distribution is unlimited
dc.description.abstractTesting of the XR-3 Captured Air Bubble Testcraft was accomplished to determine the center of gravity location which results in the minimum thrust required for a given velocity. The optimum center of gravity was determined to be one hundred and nineteen inches forward of the stern transom for velocities higher than twelve knots.
dc.description.urihttp://archive.org/details/xr3centerofgravi00lein
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.
dc.subject.lcshAeronauticsen_US
dc.titleXR-3 center of gravity characteristics.en_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentAeronautics
dc.subject.authorsurface effects ships
dc.subject.authorcaptive air bubble
dc.subject.authorXR-3
dc.description.serviceLieutenant, United States Navy
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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