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dc.contributor.authorDoolittle, James Harold, 1896-en_US
dc.date.accessioned2009-03-16T19:24:16Z
dc.date.available2009-03-16T19:24:16Z
dc.date.issued1925en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/44643
dc.descriptionThesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1925.en_US
dc.descriptionVita.en_US
dc.descriptionIncludes bibliographical references (leaves 141-143).en_US
dc.description.statementofresponsibilityby James H. Doolittle.en_US
dc.format.extent148 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.subjectAeronautical Engineering Dept.en_US
dc.titleThe effect of the wind velocity gradient on airplane performanceen_US
dc.typeThesisen_US
dc.description.degreeSc.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Aeronautical Engineering Dept.en_US
dc.identifier.oclc09378085en_US


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