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  5. Effect of stagger and decalage on biplane combinations of thick airfoils at high angles of incidence

Effect of stagger and decalage on biplane combinations of thick airfoils at high angles of incidence

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Author(s)
Medvedeff, Nicholas J
•
Sinitzin, N. N
Advisor(s)
Edward P. Warner.
Date Issued
1926
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1926.
Includes bibliographical references (leaves 13-14, first group).
Subjects
Aeronautical Engineering Dept.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
M.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
Persistent DSpace Link
http://hdl.handle.net/1721.1/37036
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