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Fuselage stress analysisReport 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.
Document ID
19930091137
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Warner, Edward P
Miller, Roy G
Date Acquired
September 6, 2013
Publication Date
January 1, 1920
Report/Patent Number
NACA-TR-76
Report Number: NACA-TR-76
Accession Number
93R20427
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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