102. Derivation of Weight Increments for a Wing Production Break at the Side of the Fuselage

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Paper Title: 
102. Derivation of Weight Increments for a Wing Production Break at the Side of the Fuselage
Year: 
1954
Paper Number: 
0102
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.

File Name: 
SAWE0102.pdf
Pages: 
15
Price: 
$20.00
Member Price: 
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SKU: SAWE0102
$20.00