Various methods for determination of principal wing load factor for which data are available; results obtained by rational methods; new expression based on equations of motion and assuming instantaneous pull up from horizontal flight at maximum velocity; recommendations with regard to load factor to be assigned to airplanes both of restricted and unrestricted classes. From thesis submitted to Mass Inst Technology.
Rationalization of load factors for aeroplane wings
Eng J
Engineering Journal ; 17 , n 12
1934
8 pages
Article (Journal)
English
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