NASA NTRS · 19930091137
Fuselage stress analysis
Abstract
Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diagonal bracing wires. Tests are conducted for landing, flying, and thrust loads.
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Warner, Edward P, Miller, Roy G. 1920-01-01. Fuselage stress analysis. https://ntrs.nasa.gov/citations/19930091137
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