102. Derivation of Weight Increments for a Wing Production Break at the Side of the Fuselage
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Paper
102. Derivation of Weight Increments for a Wing Production Break at the Side of the Fuselage. 1954.
Abstract
There is not text to this paper, rather it is a weight take of wing section of a Boeing aircraft wing section dated 5-5-1954. The value of this calculation is that it gives insight into how detailed weight takeoffs were done during the 1950’s.
