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

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Title102. Derivation of Weight Increments for a Wing Production Break at the Side of the Fuselage
Publication TypeConference Paper
Paper Number0102
Year of Publication1954
AuthorsBrown, E.
Paper Category23. WEIGHT ENGINEERING - STRUCTURAL ESTIMATION
Conference13th National Conference, Baltimore, Maryland, May 10-13
Conference LocationBaltimore, Maryland
PublisherSociety of Allied Weight Engineers, Inc.
Date Published5/10/54
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.

Pages15
Key Words23. Weight Engineering - Structural Estimation
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