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Design of a normal acceleration limiting system for a high-performance aircraft

Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1951. / Bibliography: leaves 72-73. / by William F. Bakemeyer and William H. Enders. / M.S.

Identiferoai:union.ndltd.org:MIT/oai:dspace.mit.edu:1721.1/15548
Date January 1951
CreatorsBakemeyer, William F, Enders, William H
ContributorsRobert C. Seamans, Jr., Massachusetts Institute of Technology. Aeronautical Engineering Department., Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
PublisherMassachusetts Institute of Technology
Source SetsM.I.T. Theses and Dissertation
LanguageEnglish
Detected LanguageEnglish
TypeThesis
Formatvii, 77 leaves, 6155949 bytes, 6155705 bytes, application/pdf, application/pdf, application/pdf
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., http://dspace.mit.edu/handle/1721.1/7582

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