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dc.contributor.advisorW. R. Hawthorne.en_US
dc.contributor.authorMilleville, Bertram Johnen_US
dc.date.accessioned2010-12-06T17:26:17Z
dc.date.available2010-12-06T17:26:17Z
dc.date.issued1947en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/60126
dc.descriptionThesis (M.S.) Massachusetts Institute of Technology. Dept. of Mechanical Engineering, 1947.en_US
dc.description.statementofresponsibilityby Bertram John Milleville.en_US
dc.format.extent73 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectMechanical Engineeringen_US
dc.titleGas turbine blade coolingen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineering
dc.identifier.oclc28120414en_US


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