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dc.contributor.advisorJ. C. Riley.en_US
dc.contributor.authorNeubauer, Emil T. P.en_US
dc.date.accessioned2020-10-23T18:31:51Z
dc.date.available2020-10-23T18:31:51Z
dc.date.copyright1933en_US
dc.date.issued1933en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/128166
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1933.en_US
dc.descriptionIncludes bibliographical references (leaves 49-50).en_US
dc.description.statementofresponsibilityby Emil T. P. Neubauer.en_US
dc.format.extent50 leavesen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectMechanical Engineeringen_US
dc.titleVariable compression ratio for dirigible enginesen_US
dc.typeThesisen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineeringen_US
dc.identifier.oclc35965211en_US
dc.description.collectionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1933.en_US
dspace.imported2020-10-23T18:31:50Zen_US
mit.thesis.degreeMasteren_US
mit.thesis.departmentMechEen_US


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