Show simple item record

dc.contributor.advisorChoon S. Tan.en_US
dc.contributor.authorBury, Mark Ericen_US
dc.date.accessioned2010-01-07T20:25:00Z
dc.date.available2010-01-07T20:25:00Z
dc.date.copyright1997en_US
dc.date.issued1997en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/50310
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.en_US
dc.descriptionIncludes bibliographical references (p. 172-173).en_US
dc.description.statementofresponsibilityby Mark Eric Bury.en_US
dc.format.extent173 p.en_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.subjectAeronautics and Astronauticsen_US
dc.titleInfluence of Reynolds number and blade geometry on low pressure turbine performanceen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc37896579en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record