Wing loads as determined by the accelerometer

Wing loads as determined by the accelerometer

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1924. === by James H. Doolittle. === M.S.

Bibliographic Details
Main Author: Doolittle, James Harold, 1896-
Other Authors: Massachusetts Institute of Technology. Aeronautical Engineering Dept.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2009
Subjects:
Aeronautical Engineering Dept.
Online Access:http://hdl.handle.net/1721.1/44890

Internet

http://hdl.handle.net/1721.1/44890

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