Show simple item record

dc.contributor.advisorEugene E. Covert.en_US
dc.contributor.authorDwyer, William P. (William Patrick)en_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2008-09-03T14:49:46Z
dc.date.available2008-09-03T14:49:46Z
dc.date.copyright1990en_US
dc.date.issued1990en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/42182
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.en_US
dc.descriptionIncludes bibliographical references (leaves 78-80).en_US
dc.description.statementofresponsibilityWilliam P. Dwyer.en_US
dc.format.extent194 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.subjectAeronautics and Astronautics.en_US
dc.titleMeasurement of flow boundary condition data and wing pressures in a wind tunnel test of a 45 deg swept wingen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc22926334en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record