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The stresses in stiffener openingsThe present study treats as a typical example a ring the center line of which is produced by the intersection of two circular cylinders of different diameter. Three load cases are analyzed: (1) Axial and circumferential stresses in both cylinders, the cylinder stresses themselves to be in the ratio conformal to the cylinders loaded under internal pressure. (2) Pure longitudinal tension in the large cylinder. (3) Pure shear (torsion) in the large cylinder. To simplify the calculation, it is assumed that the ring, compared to the shell, is very strong, so that its deformations have no perceptible effect on the stress condition in the shell. This provides an upper limit for the ring stresses actually produced in a shell design, for, according to the theory of stressed skin statics the shells, by elastic flexibility of the ring, regroup the forces deposited on it in such a manner that the ring is relieved.
Document ID
19930094412
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Marguerre, K
Date Acquired
September 6, 2013
Publication Date
February 1, 1942
Report/Patent Number
NACA-TM-1005
Report Number: NACA-TM-1005
Accession Number
93R23332
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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