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Unsteady airfoil pressures induced by perturbation of the trailing edge flow

dc.contributor.advisorEugene E. Covert.en_US
dc.contributor.authorLorber, Peter Fredericken_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-08-04T17:25:48Z
dc.date.available2005-08-04T17:25:48Z
dc.date.copyright1981en_US
dc.date.issued1981en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/15828
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby Peter Frederick Lorber.en_US
dc.format.extent209 leavesen_US
dc.format.extent7972957 bytes
dc.format.extent7972711 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
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/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.subject.lcshUnsteady flow (Aerodynamics)en_US
dc.subject.lcshAerofoilsen_US
dc.subject.lcshTurbulent boundary layeren_US
dc.titleUnsteady airfoil pressures induced by perturbation of the trailing edge flowen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc08068959en_US


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